LETTER TO (Sanitized)

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP66B00728R000300070003-7
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 63
• Document Creation Date: December 9, 2016
• Document Release Date: April 11, 2001
• Sequence Number: 3
• Publication Date: May 3, 1963
• Content Type: LETTER

r. 9040-63-646
Approved For Release 2 4 ' IA'-Fkl;k6, h~ R00030007000?-Ty **'Y
77 77 ~V (i
COPY J1 OF
3 May 1963
25X1A
USA?
Director 622A Program
Los Angeles, California
'ider separate cover you have received copies of a TECHNICAL
STRIP CAWSA RECONNAISSA SATELLITE which was prepared
y end submitted by Itek Corporation and its proposed Associate
Contractor, Lockheed Missiles and Space Company. Itek is vow pleased
to submit aadditi aEal Information necessary to complete its portion of
the Strip Camera Program Proposal.
Cost Proposal which identifies the various significant portions of the
program and their estimated costs. Since the submission on 22 March
1963 of our Preliminary Technical Proposal (our document no. 9040-63-
582), we have continued our joint working meetings with our proposed
meat and perform the proposed program. The second booklet conta:
data. The first booklet details our Development Plan, Work 0
and specification which describes the manner in which Itek vi
Enclosed herewith are two (2) booklets which contain these
ion to our mutual interfaces, deliverables as contained in our
ciate, Lockheed. These meetings have resulted in a more detailed
Buck Statement, and an integrated Schedule which presumes two awards of
ractual authorization to proceed by I June 1963.
The most significant changes resulting from this additional
joint effort are the change from an f/6 to on f/5 system and the inclu-
sion of the stereo capability in the initial design concept. We have
also revised the period of Itek's performance from eleven (11) to four-
(14) months, for the time of go-ahead to delivery to A/P of our
first system.
Another change from our original plan is the submission for
your consideration of an Atmospheric Resolution Tester to be installed on
the West Coast for the purpose of final, pre-flight, and photo performance
verification.
`-'Ap0roved'For Relea s 1L0 / 0 ,CIA RDP66B00728R0003000 'R X43,-7
In
OOCUM' NT NO.
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25X1A
25X1A
-646
.~f
Way 1963
our personnel are available and would appreciate the opportu-
nity to join with Lockheed Missiles and space many and present to you
a briefing in which we would describe in more detail the features of the
Technical Proposal. should be contacted for purposes
STATINTL of arranging this briefing.
proposal will meet with your approval.
Very truly yours,
ITEX CORPORATION
25X1A
rays (4)
25X1A
.> 4 w/4 each.
- 3 w/3 each.
I vfl each.
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APPENDIX A
PRELIMINARY STRIP CAMERA SUBSYSTEM ASSEMBLY LIST
a, Transport and Supply Spool Mounting
b. Forward - Diagonal Mirror and Lens Mounting
c. Support Tube - Primary Mirror Mounting
d. Shell - Corrector Plate Mounting
2. Optics
a. 'Primary Mirror and Bezel
b. Diagonal Mirror and Bezel
c. Corrector Cell
d. Corrector Plate and Bezel
3. Transport - Film
a. Supply Spool and Drive
b, IMC Drum and Drive
C. Supply and Take-up Dancers
d, Tension Assemblies
e. Auxiliary Data Head
f. Shutter and Capper
a? Cassette
b. Take-up Spool and Drive
C. Sensor Arm
5. Optical Drive
a. Roll Steering Correction
b. Stereo - Diagonal Mirror and Corrector Plate
6. Light Baffles
7. Thermal Shielding
8. Cables
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CAMERA (continued)
1) Servo Amplifier
Supply
Take-up
Metering
2) Spool Drive Assembly
Supply
Take-up
3) Metering Drive Assembly
1) Power Distribution and Control Assembly
2) S/I Control
C. Optical Drives
1) Roll Steering and Stereo Control
2) Roll Steering Drive
3) Stereo Drive
Auxiliary Data
Light-Up.Control and Lamp Adjust
e. IMC Sensor
1) Vidicon Camera and Sweep Circuits
2) Video Signal. Evaluation Unit
3) IMC Sensor Control Unit.
HANDLING FIXTURES
1. Transport Assembly and Test Fixture
2. Spool Assembly and Test Fixture - Runout
3. Cassette Holding Fixture
4. Transport Alignment Fixture
5, Spooling Fixture - Dark Room
6. Horizontal Handling Fixture and Slings
7. Strong Back ?
8. Test and Assembly Dolly
SHIPPING CONTAINERS AND PROTECTIVE COVERS
1o Camera Transit Case
2. Cassette Transit Case
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SHIPPING CONTAINERS AND PROTECTIVE COVERS (continued)
3. STM - Shipping Box
4, Structure Shipping Dolly
5. Space Mock-up - Shipping Box
6. Protective Covers
a. Corrector Plate
b, Corrector Cell - Both Ends
c. Primary Mirror
d. Diagonal Mirror
7. Thermal Unit Shipping Box
8. Protective Dust Covers
VIBRATION AND SHOCK FIXTURES
1. Lateral - Complete Unit
2. Longitudinal - Complete Unit
3. Cassette
4. Spool and Drive
5. IMC Drum and Drive
6. Transport Assembly
7. Corrector Cell
8. Corrector plate
9. Electronics Assemblies
10. Centrifuge Fixture - Camera Subsystem
11. Roll Steering Correction Drive
12. Stereo Drive
1. System -Subsystem Interface
17. Electronics Mounting and Mating to Structure
10. Supply and Take-up Dancers
11. Tensioning Assemblies
12. Complete Transport Assemblies
13. Cassette Plates
14, Roll Steering Correction Drive
15. Stereo Drive
16, Light Baffle Templates
2. Forward Structure.and Support Tube Mating
3. Primary Mirror Mounting
4. Corrector Plate Bezel
a. Corrector Plate Shell
5. Diagonal Mirror Bezel
6. Corrector Cell
7. IMC Drum to Corrector Cell
8. Supply Spool and Drive Mounting
9. IMC Drum to Drive
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TEST MODELS AND MOCKUPS
1. Structural Test Model
2. Space Mockup
3. Quarter Scale Optical Model
4. Quarter Scale Thermal Model
PATS CHAMBER AND TEST EQUIPMENT
1. Processor Test Film Cassette
2. PATS Console
3. Checkout Console Modification Unit
4. Film Incher - Transport
a. Light Jacket
5. Dummy Corrector Cell
6. PATS Chamber
,,Thermal Enclosure
sensor Layout'
Lens 'Thermal Test Enclosure
Reflector'StructuretMount
Interconnecting Cables t ,Y
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a. Test Area Layout
b. Chamber
C. Seismic Block
d. Collimator Mirror
e. Beam Splitter
f. Target Drive
g. Auto Collimator
h.. Interconnecting Cables,
Thermal Test
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APPENDIX B
STRIP CAI RA OPTICAL TEST EQUIP ENT AM TOOLING
TEST EQUIPMNT
1. Final Optical Test Stand
2. Parabolic Frame
3. Knife Assembly
4. Mirror Test Frame
5. Parabolic Mirror
6. Flat Mirror
7. Spherical Mirror
JIGS, FIXTURES AND SPECIAL TOOLS
1. Special Size Draper
2. Modified LOH's
3. Berrylium Mirror Fabrication Support (Diagonal Mirror)
4. Mirror Fabrication Support (Primary Mirror)
5. Corrector Plate Fabrication Support
Cylinder Polisher
7. Field Corrector Adapter
S. Wedgeometer
9. Large Element Cutting Fixture
12. 'Corritctor-Plate Grinding ana ro.isniug ,w&a
ii Primary Mirror Grinding Tools.
13. Mirror Polisher,
14. Aspherili g Fixture.
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APPENDIX B
STRIP CA}ERA OPTICAL TEST %=-M NT A1~D TOOLING
TEST EQUIPTENT
1. Final Optical Teat Stand
2. Parabolic Frame
3. Knife Assembly
4. Mirror Test Frame
5. Parabolic Mirror
6. Flat Mirror
7. Spherical Mirror
1. Special Size Draper
2. Modified LOH's
3. Berrylium Mirror Fabrication Support (Diagonal Mirror)
4. Mirror Fabrication Support (Primary Mirror)
5. Corrector Plate Fabrication Support
6. Cylinder Polisher
7. Field Corrector Adapter
8. Wedgeometer
JIGS, FIXTURES AND SPECIAL TOOLS
9., Large Element Cutting Fixture
11. ; Primary..Mirror Grinding Tools."''.
12.. CorrectorrPlate Grinding and Polish
.13.```Mirror.Polishers`
Aspherl sing Bixture
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 { A tl1 3-
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STEREO STRIP CAMERA DEVELOPMENT PLAN
The development of the Strip Camera System and required support
equipment has been divided into five phases. Accomplishment of these
phases is basically concurrent, however, paralleling of activity in and
between each phase has been necessary to ensure a homogeneous effort
and a unit delivery and program completion in the shortest time possible.
The five program phases are as follows:
I - Subsystem Design and Development, Test Fabrication of
Optics, and Model Units Design and Assembly.
II -- Subassembly Design and Drafting, Fabrication and
Procurement, and PATS Chamber Design, Assembly and
Installation.
III - Subassembly. of Qualification Units and Subassembly and
Subsystem Qualification Testing.
IV - Assembly and Acceptance of first two units delivered.
Assembly and Acceptance of Qualification Units as
deliverable units.
The milestone schedule on pages 6 and 7 indicates the basic spans
of effort by phase described in this plan and the proposed delivery of
the first flight unit fourteen months after program go-ahead.
PHASE I
Upon program approval, an intensive subsystem design effort will
be initiated. The procurement time for lens glass, which experience
has shown to be four to six months, dictates immediate optical design
decisions so that this key long lead item can be ordered as soon as
possible. A preliminary design freeze is therefore scheduled for two
weeks following go-ahead. In addition, this will allow for a maximum
-1-
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effort to be placed on the structural design, thermal control
considerations, and electro-mechanical control and sensor requirements.
Both a lens and mirror test fabrication program will be started as
soon as possible. The optical design requires that the optics, in
addition to being large, be of a relatively unique' configuration. The
primary mirror will be polished having a rectangular opening in its
center and the corrector lens will have a rectangular shape. Using glass
which is immediately available and having similar working characteristics,
various fabrication techniques will be tested early in the program. This
will result in an ultimate savings of both time and material. Further it
will provide necessary confirmation of details and introduce presently
unforeseen problems as early in the program as possible. Similar
fabrication and mounting tests will be conducted with quarter scale mirror
blanks. These will then become part of the quarter scale optical STRIP
model.
and verify analytical thermal computations. This thermal mock-up.will
Two models of the STRIP camera are contemplated. Realizing the
importance of the thermal problem, a scale thermal model will be
fabricated, assembled, and tested to provide early experimental results
provide direct answers for mechanical
and will greatly increase, confidence'
design.;
and structural design consideration
A quarter scale optical STRIP unit will be assembled using the test
fabrication mirrors, adapted transport and electronics assemblies and a
narrow field corrector lens. This unit,; completed in five months, will
allow basic optical testing in the presently installed DRT and provide.
hardware design answers for alignment, focus, exposure, and IMC0
PHASE II
A final interface freeze is scheduled two months following go-ahead.
This action should clarify, up-date, and confirm all interface design
parameters established by the preliminary interface freeze and allow
for a camera subsystem design freeze, The major design and drafting
-2-
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 effort will now commence to provide from the layouts the detailed parts
to be procured and fabricated. A list of major STRIP assemblies, handling
fixtures, shipping containers, environmental test fixtures, and tooling
is included as Appendix A to this development plan.
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Optical glass for the first lens is scheduled in-house during the
fifth project month. The receipt of this glass and the associated melt
data will allow for completion and final modification of the lens design
followed by fabrication of the test plates, polishing and figuring of the
lens elements, and final lens assembly and test. The first lens, based
on the cycle described, is scheduled to be complete in eleven months from
the start of the program. Previous design and manufacturing experience
with similar high acuity optical systems substantiates the time spans
here proposed.
Initial design release of the STRIP camera structure for procurement
of a structural test model (STM) is scheduled two months after go-ahead
when the final interface freeze has been established. After receipt of
the first STM in the sixth month and upon installation of mass simulation,
this structure will immediately commence subassembly,lnvironmental
qualification.
In order to provide adequate optics
optical
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testing'o
amera
will b& designed and installed at Itek,;Boston This unit :`will have'the
capability of optically testing the STRIP camera alone and as a' complete
system . under a vacuum condition of l x 10-4 inches.`. In,addition,'
provision for environmental thermal gradient testing will be provided.
A STRIP Atmospheric Resolution Tester (ART) will also be installed at
the West Coast facility. This unit would, however, not have the vacuum
and thermal test capability of the Boston PATS Chamber. Delivery of the
first STRIP Camera requires the Boston PATS Chamber to be complete in
twelve months and the West Coast ART Chamber complete in fourteen months
upon first camera delivery. The present Itek Lexington Test Facility
includes a high-bay test area containing shock and vibration test
equipment and adjoining this on one side is a panoramic camera DRT,
operational area, offices, and darkroom facility. The installation of
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the Boston PATS Chamber in the existing facility next to the high-bay
area and opposite the panoramic camera DRT is proposed and contemplated.
This will allow maximum utilization of existing equipment both capital
and project GSE.
PHASE III
The parallel procurement, fabrication, and subassembly of parts and
components for Units 1 and 2 provides both test and manufacturing
flexibility. With multiple units available, the effect of minor failures
and assembly variations is minimized. After successful qualification
testing critical subassemblies of Unit 1 are available for back-up use
on Units 2 and 3, therefore further ensuring the meeting of the first
delivery commitment.
0
The subassembly qualification teat program proposed consists of
vibration and shock testing of all significant subassemblies. The
testing will be divided into three main parts. The first is the
environmental testing of the structural test model. The second is the
environmental testing of all major electrical and mechanical subassemblies.
The third is the environmental testing of the optical and transport
assemblies. The optical test assembly will be provided 'with the optical
system that will become part of Unit 2 when the subassembly qualification
is complete. This is necessary due tothe optical fabrication ' and
assembly leadtimeand the extensive'duplication of expensive- tool in
that would be required in order to produce two optical systems in
parallel. As a result, each STRIP optical system can be produced every
6 to 8 weeks. A list of required optical test equipment and tooling is
included as Appendix B to this development plan.
PHASE IV
Actually parallel with Phase III, the production and test of Units 3
and 4 is scheduled to make maximum use of both time and facilities.
Unit 3, being the first deliverable flight unit, is gated by the
successful completion of subassembly qualification tests and the
installation and readiness of the PATS Chamber. Acceptance testing of
Unit 3 in the PATS Chamber will commence at the end of the thirteenth
project month and is scheduled for a period of one month. This allows
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EXHIBIT "A"
TO STRIP CAMERA PROPOSAL
A. Contractor shall furnish the necessary facilities, materials, and services
to accomplish the Statement of Work set forth below and make delivery to the
Government at the times and places specified herein below:
STATEMENT OF WORK
Item 1 - Design, develop, and fabricate four (4) each Stereo Strip Cameras
incorporating the four (4) GFE Stellar/Index Cameras in accordance
with Contractor's Specification No. 49849, dated 1 May 1963,
including the supplement attached thereto, said documents being
incorporated by reference, together with such changes as may be
agreed to between the Contractor and the Contracting Officer.
Item 2 - Provide mock-ups of the cameras as follows:
a) One (1) each Thermal Model Test Unit which, by scale and general
construction, simulates the Strip Camera.
b) Two (2) each Space Mock-ups which simulate the outer configura-
tion, one (1) for use by LMSC and one (1) for use by Itek.
c) Two (2) each Structural Mock-ups, including dollies, each of
which is weight and mass similation of the Camera. One (1)
for use in Contractor Qualification Program and one (1) for use
by LMSC.
Item 3 - Contractor shall furnish the following GHE and GSE:
b) Fabricate ' , two (2) each Control -arid Power Consoles.
c) Fabricate one (1) each
d) Fabricate,three'(3) each modification units for Checkout Console.
e) Fabricate two (2) each modification units for Control and Power
f) Design and fabricate six (6) each Test and Assembly Dollies.
g) Design and fabricate three (3) each interface templates.
h) Design and fabricate two (2) each Strip transit cases.
i) Fabricate three (3) each Cassette transit cases.
j) Design and fabricate 100 sets each film transit case spiders
and protective flanges and recycle.
k) Design and fabricate three (3) sets vertical and horizontal
installation fixtures.
Fabricate one (1) each Instrumentation Console.
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1) Design and fabricate one (1) each Photo Altitude Thermal Simu-
lation (PATS) Chamber including seismic block and environmental
conditioning for Boston.
m) Design and fabricate one (1) each Strip Atmospheric Dynamic
Resolution Tester excluding seismic block and environmental
conditioning for A/P.
Item 4 - Provide LMSC with two (2) additional Strip Camera cassette assemblies
for test and checkout purposes,
Item 5 - Furnish 100 film supply spools for the Strip Camera. Delivery shall
be made in accordance with the Film/Spool/Transit Case schedule
developed by the Contractor. Contractor shall provide protective
flanges for the GFE transit cases. Spools will be recycled.
Item 6 - Furnish necessary field engineering services to support the cameras
at LMSC and VAFB in accordance with Detailed Field Engineering and
Flight Support Work Statement, dated 14 May 1962.
Item 7 - Contractor shall furnish spares in accordance with the following:
a) On or before the eighth (8th) contract month, Boston shall furnish
the Systems Engineering Contractor (SE) seven (7) copies of a
production list containing the part number, description, and
quantity of those parts deemed necessary by Boston to support
the equipments after shipment from Boston, considering the deliv-
ery schedule and two (2) facilities.: This list shall indicate
those long-lead-time items already released to support the equip-
ments. Subsequent lists,"if_necessary, will be submitted on a
monthly basis.
If within thirty (30) days from-the date of submission, the SE
.and the Customer has neithor;approved nor disapproved all-the
items contained in such production lists, those items shall be
deemed to have been authorized for provisioning purposes. In
the event items.,are disapproved by the Customer, procurement
activity shall be terminated where necessary.
c) Spares shall be shipped to the Associate, F.O.B. the Associate's
facility for maintenance of accountability in a segregated Stores
Area. The parts shall be available to Boston's Field Engineering
and Flight Support Group to replace those parts as may be neces-
sary to certify flight readiness of the cameras.
d) The costs, fee, and delivery schedule of these spares shall be
determined at a later date.
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Item 8 - Contractor shall perform Inspection, Qualification and Acceptance
tests in accordance with Specification No. 49849, and the following:
Item 9' Contractor shall furnish the following reports and attend required
shall be at Boston. The Systems Engineering Contractor (SE)
and other Customer's representatives will be notified five (5)
days prior to the beginning of final acceptance tests. These
tests shall be administered in accordance with the approved
Acceptance Test Procedures. Requests for waivers on end item
equipment deliveries shall be submitted to SE/TD for resolution.
The execution of a DD Form 250 by Itek, which may contain con-
currence signatures of SE and other Customer's representatives,
shall constitute final acceptance. Copies.of the DD Forms 250
will be forwarded to the Contracting and Finance Officers.
All Qualification Test Specifications and Procedures (QTS/QTP)
shall beprepared by the Contractor and the`QTS shall be approved
by SE/TD prior to the performance of.the Qualification Test The
a) Inspection of the material to be delivered from Boston shall be
at a level deemed necessary by Boston and approved by the Govern-
ment to insure performance. Boston shall provide additional
inspection services in the event performance verification or
rework is necessary to such material after acceptance and
delivery. Boston shall also verify that no damage in transit
has occurred to its materials after shipment from one facility
to another.
b) Shipment is F.O.B. Lexington, Massachusetts, via such carriers
and to such destinations as may be designated by the customer.
Boston will provide instrument transit cases.
c) Final acceptance of equipment and materials to be delivered
b) Monthly TWX Financial Report - to be forwarded the 20th of each
month for the preceding Boston accounting month.
c) Weight Report - to be forwarded every two (2) weeks to the
Systems Engineering Contractor showing the current weight estimate
and first and second moments of inertia. Should the details of
the report be unchanged, a TWX statement to that effect will be
forwarded in lieu of the report.
Weekly TWX progress report - to be forwarded to SE/TD on Wed-
and shall report significant highlights of development
for the preceding week - ending Saturday.
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,..Calibration data.
These drawings may be red-lined.;
Strip Camera Electrical.Sc.hematics as wired (three
each Strip. Camera'consisting'of:
nately at Associate and Boston Such meetings shall be chaired
and minutes prepared and distributed by the Systems Engineering
Contractor. Contractor shall present such briefing aids and
data as required.
Provide the Systems Engineering Contractor with documentation of
d) System Qualification Test Report - to be forwarded to the Systems
Engineering Contractor two (2) weeks or sooner after completion
of each major test phase (i.e., System shake, System photo/thermal/
altitude, etc.). A consolidated, summarizing report shall be for-
warded forty-five (45) days after the System Qualification Test
Program.
e) Subsystem and Subassembly Qualification Test Reports - to be
forwarded to SE/TD two (2) weeks or sooner after completion of
each major test phase. A consolidated, summarizing report shall
be forwarded forty-five (45) days after the Subsystem Qualifica-
tion Test Program.
f) Acceptance Test Reports - to be forwarded as part of each Camera
logbook.
g) Post-flight Engineering Analysis Report - ten (10) copies to be
forwarded to SE/TD upon completion of each analysis. LMSC will
furnish Contractor with copies of all pertinent telemetering
data obtained during flight for engineering analysis by Con-
tractor of camera performance.
h) Systems Engineering Meetings shall be held once each month alter--
`1. Strip Camera Logbook.*
Results of Acceptance Tests.
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Delivery - Based on a contractual go-ahead of 1 June 1963 the Contractor shall
deliver the work called for above in accordance with the following schedule.
Unless otherwise specified, acceptance and inspection shall be at Contractor's
plant or plants of shipment made F.O.B. Contractor's plant, Lexington, Massa-
chusetts.
Item 1 - Strip Camera, four (4), (less supply spools) (including Cassettes).
Serial No. 3 1 August 1964
Serial No. 4 1 October 1964
Serial No. 1 1 December 1964
Serial No. 2 1 February 1965
Item 2 - a) Model Test Unit (Boston)
b) Space Mock-up, Strip Camera - two (2) each - (Boston) 15 October
1963 - (A/P) 1 November 1963.
c) Structural Test Model, Strip Camera - two (2) each, including
dollies - (Boston) 3 January 1964 - (A/P) 2 March 1964.
Item 3 - Contractor shall deliver GHE and GSE as follows:
A P B Date
mentation Console.
a) Fabricate one (1) each Instru-
b) Fabricate two (2) each Control 2 31 January, 1964
Fabricate one (1 33 April 1964
) each TM =,
Fabricate;;threa" (3) , sac
Modification unite tor
Fabricate two (2) each Modifi-
Power Consoles.
cation units for Control and
f) Design and fabricate six (6)
each Test and Assembly
Dollies.
g) Design and fabricate three (3)
each interface templates.
14 February 1964
28 February 1964
(2)
1 April 1964
1 May 1964
2
1 August 1964
1 October 1964
31 January 1964
(3)
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 Approved For ReleSRdE1Q/EA&-RDH6&OTYE000CR03-7,
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h) Design and fabricate two (2)
each Strip transit cases 2
i) Fabricate three (3) each 3
Cassette transit cases.
j)
Furnish
transit
100 sets each
case spiders
film
and pro-
tective
flanges and recycle.
k) Design and fabricate three (3) 2 1
sets vertical and horizontal
installation fixtures
1) Design and fabricate one (1)
each Photo Altitude Thermal
Simulation (PATS) Chamber.
m) Design and fabricate one (1)
each-Strip Atmoopperic Dynamic
Resolution Tester.
Item 4 - Two (2) Cassette Subassemblies
Item
Case Plan
Date
1 August 1964
1 October 1964
16 March 1964
15 April 1964
1 August 1964
1 June 1964
1 August 1964
1 October 1964
3 August 1964
16 March 1964
-15 April 1964
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Item 6 MField Engineering Services`shhal be fuurrnis d as required or the '
period of performance,'of this Contract, contemplated to be thrbugh
428 May... 1965.
Item 7` Spare, parts shall be delivered in accordance with Item 7 of'Para-
graph A of this Work Statement.
Item 8 - Qualification, Inspection and Acceptance shall be performed in
accordance with Item 8 of Paragraph A of this Work Statement
Item 9 - Reports:Deliver in accordance with a. through i..of.Item 9 of
Paragraph A of this Work Statement.'
- Film Supply Spools
Per Integrated Spool/Film/Transit
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
SPECIAL HANDLING
 Approved For RelaP2F'IAA k0A6+A-RM86n07Q090'3U7%03-7.
C. Furnished Equipment
Item Description
1. Film and film transit cases as re-
required for testing and checkouts
2. Stellar/Index Cameras, four (4),
including Transit Cases, Supply
Spools and Stellar/Index Cassettes.
3. System outer skin, Fairing Subassembly,
adapter, and other parts suitable for
Camera qualification.
4. Contractor will be furnished and is
also authorized to use on a no-charge-
for-use basis such items as special
tooling, test equipment, ground handling
equipment, ground support equipment,
and facilities generated under Contract
BT-1.943 and any other contract between
the parties hereto.
Location Delivery Date
A/P 1 August 1964
1 October 1964
1 December 1964
1 February ,1965
Boston 3 July 1964
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
SPECIAL HANDLING
 Approved For Relea
Jrc%?IMML I1MNULINLI
SYM DESCRIPTION
Specifications Procedures
Engrg
Engrg
f'r~ject.
App' d
SEA 'd
1 r P Approved For
LSYsued 1 May 1963
.SPECIFICATION FOR
STEREO STRIP
AND STELLAR/INDEX
CAMERAS
-RD~P66B00728R0003000 0003-7
. HANDLING lCode
DATE APPROVAL
Sheet 1 of 25
 SPECIAL HANDLING
Approved ror ease - DP66B00728R000300070003-7
1.0 SCOPE
1.1 Objective: This specification covers the requirements for a
high-acuity StereB Strip Camera and associated stellar/index cameras.
The camera is to provide programmed vertical and stereo photographs at a
resolution level of 2 feet or better from 90 n. miles. The system is to be
designed to be used in a light-tight structure and will allow recovery of the
film only.
2.0 APPLICABLE DOCUMENTS
2,1 The following publications of the issue in effect as of date of
issue indicated, shall form a part of this specification to the
extent specified herein. In the event of conflicting provisions, the
requirements of this specification shall prevail. See Appendix A.
Specification
Number
Title
Date of Issue
MIL-STD-150A
6117B
MIL-E-ID
Photographic Lenses
Environmental Test, Specification
Electron Tubes and Crystal
Rectifiers
12 May 1959
1 July 1960
31 March 1958
447969A
Systems Electrical Interface
Specification
9 April 1962
1072045A
Cable Design Control Specification
8 December 1960
SP2-156
Electrical Interface
10 May 1962
:49900
Interface Drawing
Spooled Film - 12"
Semi-Conductor X-Ray Inspection
3..0 REQUIREMENTS
3.1 General
3.1.1 General Requirements: The cameras shall conform to the
requirements of this specification.
3.1.2 Parts, Materials, Processes: Shall be consistent with flight
objectives and good design practices. When and where
applicable, MIL standards and specifications for space equipment shall be used
as a guide.
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS 4 9 8 4 9
Approved For elease 2001/04/20 : CIA-RDP66B00728R00 1300070003-7
SPECIAL HANDLING Sheet 2 of 25 Shpot
 SPECIAL I-IANL)LINU
Approved ror e 0300070003-7
3.1.3 Weight: Total weight of the Stereo Strip Camera including
empty sppply spool but excluding cassette shall not exceed
975 pounds. Maximum film capacity will be 80 pounds. The cassette shall
not exceed 20 pounds. A stellar (attitude)/index (terrain) camera is provided
for an additional 15 pounds.
3.1.4 Identification: Itek nameplates including main assembly
part number and serial number will be supplied. The name
"Itek" will not be indicated.
3.2 Selection of Specifications and Standards
3.2.1 Standard Parts: AN or MIL standard parts shall be used
wherever possible.
3.2.2 Commercial Parts: In applications for which no suitable
corresponding AN or MIL part exists or where they are not
readily available, qualified commercial parts may be used.
3.3 Material
3.3.1 Metals: Metals shall be of the non-corrosive type or be
suitably protected (subject to the thermal requirements)
to resist corrosion during maximum service life, (Test, storage, and flight.)
3,3.2 Semi-Conductors: To aid in establishing a ground rule
philosophy in semi-conductor selection, the following guides
3.3.2.1 Requirements and characteristics of MIL-E-1D must
be considered minimum, and no component shall be
used that is.notvendor-certified or tested to the, limits of that specification.
3.3.2.2 The. environmental requirements of 6117 may be used
as minimum levels, provided sufficient de-rating
is applied to verify thermal competence.
3.3.2.3 All semi-conductors must be X-ray inspected per
TD-55.
3.3.2.4 All electronic packages containing semi-conductors
must be aged under simulated load for 200 hours
3.3.3 Electrical: Interface power and power distribution
characteristics shall be as specified by 447969, System
Electrical Interface. 447969 shall be used as a guide for Camera System power
and signaldistribution, shielding, and grounding.
3.4 System Design Objective: The camera subsystem shall satisfy the
high-acuity Strip Camera concept and shall also include a stellar
Approved For
TITLE
SPECIFICATION FOR STEREO STRIP
D 6B00728R00 300070003-7 4 9 8 4 9
e ease 2UV1~'Oi XC VA-
SPECIAL HANDLING
 SPECIAL HANDLING
!001"4/20 : CIA-RDP66BOO728ROO0300070003-7
(attitude recording)/index (high resolution terrain) camera, and a take-up
cassette which will be independently mounted in a recovery capsule. Electrical
circuits, controls, and cycling programmer capable of operating on commands
from the vehicle programmer shall be included. Instrumentation which will
provide inputs to the vehicle telemetry system to monitor critical functions
of cameras while in flight will be established as indicated in SP2-156.
3.4.1 Photo Quality: Strip photographs will be of such quality
as to permit the resolution of an adequately illuminated
Air Force test pattern at a level of 72 1/mm. Tests shall be conducted for
qualification and acceptance of equipment using an Air Force test pattern of
the type defined in MIL-STD-1500 Target contrast shall be that required to
present 2:1 contrast at the camera.
3,4.2 Location Accuracy: The system design objective for location
accuracy of any point on the Strip photograph shall be
of + 1/10 mile.
3.4.2.1 Time recording to an accuracy of 10 milliseconds
will contribute a maximum uncertainty of + 1/20 mile.
3.4.2.2 Positioning of the optical axis to within + 15
minutes of arc will result in a possible error
3,4.3 Lifetime: The mission life will be one to four days during
which photographs can be taken at intermittent times.
3.4.4 Swath Width: The Strip Camera shall provide ability to
photograph selected target. areas having a nominal swath
width of 6.9 n. miles at an altitude of 90 n. miles and having photographic
quality per-paragraph 3.4.1.
3.4.5 Roll Positioning: Roll positioning of the camera will be
provided for selection of targets not directly beneath
the flight path. The maximum roll angle to be provided will be 30 degrees.
A signal indicating the angle of roll with respect to vertical will be
provided in discrete positions of increments to allow correction of the
IMC system and to film-record the roll angular command in the auxiliary data
block of the S/I unit. The nominal response time for roll positioning shall
be 30 seconds from -30 to +300 roll.
3.4.6 Continuous Cover: Once placed in operation, the camera
shall have the ability to operate in a continuous manner
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX GAMJKAS 4 9 8 4 9
Approved For elease 2001/04/20 : CIA-RDP66B00728R00 1300070003-7
18 n. miles length (from 90 n. mile altitude).
will be provided accomplishing a strip stereo pair of
for a maximum of 20 minutes during the mission duty dycle.
3.4.7 Stereo: Fore and aft stereo with 120 stereo convergence
SPECIAL H Ai-ofl1 suit. Sheet 4 f 25 Sheers
 Approve or Release 20 / i/'Z CU-R P 6 R000300070003-7
3.4.8 Programming: The orbital programmer will be used for
commanding operation.
3.4.9 Environmental Performance: The camera subsystems shall
perform within the limits established in this specification
when exposed to any natural combination of the environments specified.
3.5 Vehicle, System Characteristics, and Interface
3.5.1 V/h for IMC: Ground selection of a suitable time varying
V h ramp will be required via real time command. The
system will be capable of accepting commands in the V/h range .02 to .06
radians/second and will accomplish IMC. A minimum of 10 ramps will be
provided. These ramps will be adjusted prior to flight to narrow the design
V/h range for improved V/h accuracy. Ramp repeatability, once set, shall be
one (1) percent, The system shall be capable of operating during either
increasing and/or decreasing V/h conditions using a cosine ramp.
3.5.2 Vehicle Stabilization Requirements (1.65 values)
3.5.2.1 Angular Deviations
Roll + k degree
Pitch + k degree
Yaw + 1/3 degree (corrected for earth's rotation).
Capability to change the yaw of the vehicle from 0 to 3.6 degrees at a rate
of 0.16 degree/minute commensurate with the inclination angle will be provided
by the associate.
3.5.2.2 Residual Angular Velocities
Roll 3?/hr.
Pitch 9?/hr.
Yaw -3?/hr.
3.5.2.3 Momentum Balancing: No momentum balancing is to
be provided.
3.5.3 Camera Compartment Environment:
3.5.3.1 Pressure: The camera compartment will be
unpressurized.
3.5.3.2 Temperatures: During photographic operation,
temperature of the Strip Camera shall be maintained
at 70 degrees F + 10 degrees F. Gradients on the take-up cassette ranging
from 20 degrees F to 180 degrees F can be expected during recovery. Gradients
and transients affecting optics and structure maintaining focal length will be
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS
4
9 8
4 9
A
roved For
eleas
0
1104/200 : IA
-R
DP
66
O7
28R00
130070003-7
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9
,
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Sheet
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of 25
Sheets
 Approved For Release 2mr/LIA[0rN00300070003-7
controlled to tolerable levels,by thermal design. Thermal design shall:
a. Establish uniform ambient temperature of
optics and structure to aid in maintaining
focus using passive thermal control wherever
possible.
b. Minimize optical component temperature
gradients,
c. Provide cooling for camera electronics and
electromechanical devices.
d. Provide thermal protection for the film near
heat sources greater than 150 degrees F and
maintain thermal stability of film areas.
To assure stable operational temperatures, emissive coatings and thermal
insulation will be applied on those areas of the camera structure and
components as shall be mutually agreed upon by Itek and the associate.
Specific power dissipating components and temperature-sensitive components
or subassemblies shall be the subject of special consideration for negotiation
by the associate contractors with System Engineering.
3.5.3.3 Light-Tight: The associate structure which serves
as a camera compartment will be constructed in such
a manner as to prevent light other than image forming light from falling on
and exposing the film at any time. Light boots within the camera to meet
this requirement will be provided by Itek.
3.5.4 Auxiliary Data Film Record
3.5.4.1 Time Signal: A digital clock (associate-furnished)
will operate in conjunction with the camera subsystem
by supplying signals for illumination of 29 lamps in the.data block of the
stellar/index camera and will be used for time recording on the edge of the
strip format. It will be capable of storing time unambiguously for a period
of 5 days in increments of 0.01 second or less, A readout will be provided
to transfer the.clock reading to the film once per. stereo pair, and a serial_j
binary readout will be provided to transfer the clock reading via the
telemeter. The clock error will not exceed 10 milliseconds in any 12-hour
period after accounting for clock drift and offset. Serial clock readout
will be put on strip photography under the mask.
3.5.4.2 Roll Steering: Lights indicating roll angle image
motion correction will be provided in the S/I data
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS
Approved For ele 20 / 20 : F7,a( 4'28R00 -
t L~ ~ufC m/ M.. f~.i }1 P P Y W o f 7rf :-i n P Y c
 SPE'r.,iAL HLI .IDLING
.3.5.4.3 Attitude Information: The stellar camera, of the
stellar/index camera subsystem will supply photo-
graphic records of roll and pitch positioning to 0.1 degree accuracy.
3,5.5
Electrical Power: SP2-156 delineates
nectors that shall be provided.
3.5.5.1 Electrical Power (Maximum):
V/h
Cassette
Heater
Re
Ca
Av
Du
quired
mera
g. Pwr.
ring
Total Available
Energy During
100/hr. Flight
Power Source
Generator
Power
op
erate
incl. Heaters
Plus 22.00 to
plus 29.25 VDC
unregulated
300w
1900 w/hrs.
Plus 28.3 VDC
plus or minus
2.0 percent
regulated
50w
1875 w/hrs.
Minus 28.3 VDC
plus or minus
2.0 percent
regulated
25w
125 w/hrs.
115V plus or
minus 1 percent
lOw for
40 min.*
35w
80 w/hrs.
single phase
400 cps plus or
minus.O.02
percent
*as.programmed.
3.5.5.1.1 Starting Transient: Maximum starting
transient load on the unregulated DC
supply shall not exceed 500 watts and shall be limited in duration to a
maximum of 1 second at the beginning of each operate period,
of unregulated DC not
operation.
3.5.5.1.2 Recurring Peaks: Maximum recurring
peaks shall not exceed 500 watts
exceeding 500-millisecond duration during camera
3.5.5.1.3 Noise Level: Past experience has
indicated that considerable noise may
be present in these sources. All electrical circuits and controls should
TITLE
SPECIFICATION FOR STEREO STRIP
Approved For elease 2& 4/28--X0-RDP56 BOO7A28(/ROO 300070003-7 4 9 8 4 9
SPECIA s. : e 9,~~f~`CDLING Chonr- 7 of 2L55 CF.nnrc
 Approved ran
be designed to be capable of operating the the presence of noise as high as
2.0 V (peak-to-peak) due to 2,000 cps regulation on the plus and minus
regulated DC power supplies. Transients of + 10 volts of 10-millisecond
duration may be experienced.
3.5.5.1.4 Ascent Phase: If required during ascent,
the vehicle will supply 50 watts of
+28 volt unregulated power continuously and 150 watts of +28 volts regulated
power immediately after launch to the camera subsystems. Should this power
be required, all tests will be performed under simulated conditions of power.
3.5.6 Prograamner: Camera ON/OFF operation, V/h programmer
synchronization, max./min. exposure, discrete roll positioning
command signals and stellar/index ON/OFF commands shall be provided by the
command programmer.
3.5.7 Commands: Signals for the operation of the equipment must
be obtained. The operation signals to be provided are as
COHMAND SIGNAL SOURCE LOAD
ON/OFF 1 relay 1 amp. max.
V/h - IMC - Selection of Command link 24-volt stepping
best time function for switch coil
internal V/h approximation.
A pulse train signal will
make this selection via
real time command.
V/h Generator C, and
1 relay
1 amp. max.
(ON/OFF)
Max/Min Exposure Selection
1 relay
1 amp. max.
Stereo/Mona
1 relay
1 amp. max.
Roll Steering IMC
binary-coded
1 amp. max.
control (during time
relays
camera rolled)
Stellar/Index Inter-
1 relay
1 amp. max.
valometer Command
(ON/OFF)
3,6 Desi n: The Strip Camera is intended to provide high resolution
photography of selected target areas. It is an integral system
whose operation shall be sequence-programmed and automatic upon command,
including film transport, IMC, and auxiliary data recording. The basic
design utilizes a focal plane containing moving film with IMC accomplished by
rotation of the drum proportional to V/h.
TITLE
SPECIFICATION FOR STEREO STRIP
4 9 8 4 9
Approved For R
M%eS M/27( DUA 00728R000
00070003-7
 , ' SPECIAL HANDLING
Approved or Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
3.6.1 Configuration: The design of the camera shall be such so as
to permit installation in an envelope as defined by Drawing
3.6.2 Mechanical Interface: In accordance with Drawing Number 49900.
3.7 Construction: Within the limits of weight and space available,
construction techniques, processes, and materials shall be selected
to provide the maximum in structural integrity for the environment to be
encountered.
3.7.1 Suspension: The principle parts of the camera shall be
designed for the,Strip Camera to be operated as an integral
unit. The principle parts of the camera are the primary mirror, the 450
mirror, the aspheric corrector plate, refracting correction assembly, roll
steering IMC compensator, IMC drum and drive, slit width control, and film
transport mechanism including supply spool, film "dancer" loops and associated
parts and drive mechanism, and a take-up cassette including spool and drive
located in the recovery capsule. The Strip Camera shall be supported by the
external skin of the vehicle and held in such a way to maintain alignment with
the cassette and the stellar/index subsystem.
3,7.2 Maintaining Focus: The structure shall establish and maintain
the distance from the nodal point to the film to the accuracy
required to attain the specified resolution. Construction of the structure
maintaining focal length shall ensure that the spacing to the film will not be
changed due to launch acceleration, vibration, and shock. The construction
and materials shall maintain focus during and subsequent to the uniform
ambient temperature variations. expected.
.3.7.3 Film Thermal Shielding: Film paths and equipment near
..high-temperature external skin shall be properly thermally
shielded if required
3.8 Performance
3.8.1. Photographic Quality: The high-acuity Strip Camera, when
operated, will produce a minimum degradation of static
,optics/film resolution. The design objective shall be 90 percent of the
static LWAR optics/film resolutions obtained on the optical test collimator.
The camera shall produce photographs with an LWAR resolution of 70 lines/mm
or greater when operated under simulated flight condition utilizing the DRT
with moving 2:1 contrast Air Force test pattern as defined in MIL-STD-150.
(LWAR-AWAR for linear aperture) Target contrast shall be that required to
present 2:1 contrast taN_?the camera.
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS 4 9 8 4 9
Approved For elease 2001/04/20 : CIA-RDP66BOO728ROO(I-InnnZO003-7
Lr. G Sheet '9 of 25 Sheets
 SPECIAL. HANDLI
3.8.2 Image Motion Compensation Accuracies: The image motion
compensation mechanism and drive system shall have
performance compatible with the design requirement pertaining to photographic
quality.
3.8.3 IMC Drive Smoothness: The IMC drive system shall be smooth
such that no objectionable bandingooccurs on the photography
of ground scenes. For measurement purposes, the amount of banding present
will be determined using aastable diffuse DC light source or a strobe light.
3.8.4 Exposure Control Evenness: Banding caused by non-uniform
IMC motion or slit variations shall be controlled to
produce less than 0.15 Log E change in exposure. The Delta Log E exposure
change shall be determined by reference to the straight-line portion of SO-132
sensitometric control film printed and normally processed.
3.9 Major Components: The high-acuity Strip Camera shall consist of:
3.9.1.1 Base: The camera shall be designed to utilize
80-132/206 or equivalent thin base (000035-inch)
polyester film. Use of polyester materials varying in thickness between
1.8 and 4 mils will be a design objective.
3.9.1.2 Emulsions: The camera will be capable of handling
and exposing Eastman Kodak films Special Order
132/206 or other films'havingequivalent or better photographic emulsions and
physical properties.
3.9,1.3 Width: The system will use 12-inch wide film.
3.9.1.4 Spooled Film: The spooled film shall be in
accordance with Itek Specification
3.9.1.5 format:. The format will be in accordance with Itek
Drawing Number
3.9.2 Film Transport System: Film will be stored on supply and
take-up spools. During camera operation, these spools will
be driven at essentially constant speed which will be determined by the
required cycling rate. (Proportional to V/h.) An INC drum will meter
unexposed film. The film on the drum will be held under tension during the
photography. Dancer loops will be utilized to maintain tension and serve to
decouple the IMC drum from the spool drives. Supply and take-up spools will
be controlled in a manner to maintain the proper amount of film in the dancer
Approved For
TITLE
SPECIFICATION FOR STEREO STRIP RAS e DaSTELLAR/INDEX ICOA-AR P R00 300070003-7 4 9 8 4 9
 SPECIAL HANDLING
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
loops, thus preventing slack loops or excessive film tensions. The film path
will be designed to ensure proper tracking of the film and to eliminate the
possibility of film tear or damage to the emulsion. The film transport system
will be designed to minimize static discharge in the active format area in
aerial scenes.
3.9.2.1 Allowance for Film Splices: The film handling
system and guides shall be designed to allow for
smooth passage of the required number of proper film splices expected in
each roll of operational film. The film transport shall be capable of passing
film that has been properly butt-spliced with 1-inch wide polyester film tape
(Minnesota Mining and Manufacturing Company, Type Number 850 or equivalent).
3.9.2.2 Rollers: All rollers in the film transport
mechanism shall be consistent with good design
practice determined by the type of film to be used. A minimum diameter of
one inch shall be used wherever possible.
3.9.2.3 Film Loading: The camera shall be capable of
being loaded in subdued light using live film
protected by 30 feet of leader.
3.9.2.4 Camera Start: From the time the start sequence
command is received, the camera system shall be up
to speed in approximately two seconds.
3.9.3 Supply and Take-up Spools
3.9.3.1 Capacity: Approximately 80 pounds (3,300 feet) of
thin-base Estar 12-inch film (3k mil).
?3.9.3.2 Interchangeability Spools will be removable and
.interchangeable between cameras.
3.9.3.3 Fl anges: The flanges will be removable from the
hub.
3.9.4 Cassette
3.9.4.1 Basic Design: The cassette will consist of the
take-up spool and film take-up drive system for
the Strip camera mounted in a unit structure to allow installation in the
recovery system. The Strip take-up spool and drive shall be controlled by
the Strip camera film transport mechanism. Consideration will be given in
the cassette design for spool removal in dark conditions. The total power
consumption of the cassette shall be held to a minimum.
Approved For
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS
Relea&Roaftt0 : jgIi_ 16 ~,28R00
3300070003-7 4 9 8 4 9
Sheet 11 of 25 Sheets I
 SPECIAL HANDLING
3,9.4.2 Configuration: The design of the cassette will
conform to the basic configuration and space
limitation as shown by Drawing Number J Provision will be made for
mounting the cassette within the vehicle in accordance with the mounting
provisions as shown in Drawing Number
3.9.4.3 Instrumentation
3.9.4.3.1 Thermal Instrumentation: One Ruge
BN 2400 resistance thermometer will
be installed in the cassette.
3.9.4,3.2 Remote Film Footage Indication Requirement:
The take-up spool shall be provided with
a transducer and the necessary electrical connections to permit remote
indication of the amount of 12-inch film that is on the take-up spool at any
time during the operation. This shall be accurate within 5 percent over
total spool radius,
3.9.4.4 Design Requirements:
3.9.4.4.1 Cassette Weight: The weight of the
complete cassette with empty spools
without film shall be held to a minimum and shall not exceed 20 pounds.
3,9.4,4.2 Film Loading: The cassette shall be
assembled with polyester leader attached
to the spool and threaded through the film handling system with six feet of
leader external to the cassette film entrance slot. This leader shall be
spliced to the camera film for final assembly and testing purposes.
3.9.4.4.3 Film Capacity: The cassette shall
contain a film spool of special design
with a minimum diameter core and a maximum film capacity.
3.9.4.4.4 Strip Anti-Backup Device: The cassette
shall be designed to incorporate a
brake in the spool drive system to prevent the take-up spool from unwinding.
This brake shall be capable of being released for test and checkout purposes
by applying 28 volts DC on an appropriate pin connection. The brake shall
be mechanically engaged when the voltage is removed.
3,9,4.4,5 Cassette Heaters: Any required heaters,
to maintain 70 + 10 degrees F as may be
specified by SE, shall be Itek's responsibility, The heater circuit will be
on unregulated DC. Heaters will be controlled by an internal thermostat.
Heater power will not exceed 15 watts.
TITLE
SPECIFICATION FOR STEREO STRIP
- 4 9 8 4 9
Approved For R f SZ00'f/04120: INDEX CAMERAS
ease CIARDP66B00728R000
SPECIAL H NDUNC; Cvnnr ,? F 9s c ,,,...
 SPECIAL HANDLING
Approved or Release - 0003-17
3.9.4.5 Strip Take-up Performance: The take-up shall be
capable of taking up the required amount of film
as specified and shall be able to be started and stopped at least three
hundred times during the taking up of a complete four-day roll of film under
simulated duty cycle. The acceleration time shall be such that no slack loop
will be formed during camera system operation. Film tension shall at all
times be maintained.
3.9.5 Optical System: Specification MIL-STD-150 shall be used as a
optical system,
guide in the design, manufacturing, and testing of the
3.9.5.1 Optical Characteristics: The optical characteristics
shall meet the photo quality requirements of
paragraph 3.4.1 when using the photographic film supplied per paragraph 3.9.1.
3.9.5.2 Optics - 150" f/5: The resolution shall approach
diffraction limited performance at high contrast.
Each lens will have focal length of 150 + 0.75 inch. Custom assemblies may
be required and hence need not be interchangeable. The focal length will be
maintained at operational altitude and temperature of 70 + 10 degrees F (see
paragraph 3,5.3.2),
3.9.5.3 Mirrors: Every effort shall be made to minimize
temperature gradients through thermal design,
specifying shielding, etc.
3.9.6 Photographic Filter: A photographic filter shall be mounted
in the. optical path. This filter shall not degrade the
photographic image when the'camera is used for its intended purpose. The
filter shall be of the proper value for the selected film emulsion to be used
as a haze filter (similar to Wratten 12).
3.9.7 IMC Drive: An IMC drive and shutter mechanism will be
provided to drive the film past the exposure slit. Speed
will be proportional to V/h. IMC speed during exposure will be held
constant to meet the requirements of paragraph 3,8.3 and 3.8.4 to provide
good positional determination and to minimize IMC error,
3.9,8 Image Motion g2Mensatian The cameras will be
designed for a median V /h - .04 (Range .02 - .06) radian/
second. Upon receipt of proper IMC function selection, the system will
compensate for ground motion,
3.9.9 Exposure: Exposure shall be accomplished by utilizing a
focal plane shutter. Exposure time may be varied by command
between a choice of two slit widths which are selectable on the ground within
the design range.
Approved Ford
TITLE ,
SPECIFICATION FOR STEREO STRIP
Release Release OX ClA-RDP66B00728R0
 ~rc~.IML M~ L)LING
3.9.10 Vector Detector: An image motion detector will be provided
to sense relative motion. The along track signal will trim
IMC drum speed to its correct value and a cross track signal will be derived
to be furnished to the vehicle for yaw correction. 9. V/h or better is the
specified accuracy.
3.9.11 Telemetering Data Transducers: In accordance with SP2-156
Electrical Interface.
3.9.11.1 Thermal Instrumentation: Ruge BN 2400 resistance
thermometers or equivalent will be installed in
the camera to monitor the temperatures of critical structures and components.
Temperature sensors shall be located as mutually agreed upon between Systems
Engineering and associate contractors.
3.9.11.2 Functional Instrumentation: As defined in SP2-156,
Electrical Interfaced Instrumentation will be
re-identified and may be substituted.
3.10 Stellar/Index Camera Subsystem
3.10.1 General: Itek shall supply a Stellar/Index Camera subsystem
under separate contract. This subsystem will provide a
photographic record to permit indexing and correlation of the Strip
reconnaissance photography with local mapping systems by image matching.
A simultaneous star photograph will permit accurate determination of vehicle
attitude. A time label shall be recorded with the index format. LMSC shall
provide a 29-bit time word to the (stellar/index) camera from the digital
clock upon interrogation by the camera.
3.10.2 Stellar Index Control and Programming: The associate shall
provide a signal to initiate and continue operation of the
Stellar/Index Camera Subsystem, as required throughout the mission. The
Strip camera'will act as the intervalometer, proportional to V/h, and provide
all subcycle commands required by the stellar/index camera, whether or not
photography is being accomplished. Stereo/index photography will be
accomplished at a ratio adequate to insure nominal 557. overlap.
TITLE
SPECIFICATION FOR STEREO STRIP
Approved For R c'Ab /1P Ik B00728R000 00070003_7 4 y o 4 y
SDrrii, I 1 4 r _. ._ I chnnr ..F 9C;
 4.0
TEST REQUIREMENTS
4.1
General: The tests listed are to be performed in accordance
with the requirements stated within this specification.
4.1.1
Test Location: Itek Laboratories, Lexington, Massachusetts,
4.1.2
Witnessing of Tests:
Tests may be witnessed by the
following:
Systems Engineering Contractor (SE)
Itek-authorized representatives
Other personnel designated by customer,
4.1.3 Records of Tests and Reports: Test data shall be recorded,
The contractor shall prepare test reports covering the
results of tests required in this specification referencing the results of
each test to the applicable test specified herein.
4.1.3.1 Camera Subsystem Qualification Test: All
qualification test results shall be reported
to the Systems Engineering Contractor, giving in detail all failures, repairs
necessary, and malfunctions not resulting in failure. "Failure" is defined
as being caused by the camera and "malfunction" is defined as being caused
by GSE, personnel, procedure deviation, etc.
4.1.3.2 Subassembly Qualification: Reports on subassembly
qualification tests shall be submitted to Systems
Engineering Contractor and the customer.,
4,1.3.3 Acceptance Test: .The acceptance test shall be
reported to the Systems Engineering Cont{actor.
4.1.4 Test Conditions: Applicable test conditions specified in
6117 shall be used.
4.2 Classification of Tests:' Inspection and testing shall be
classified as follows:
4.2.1 Qualification
4.2.1.1 Camera Subsystem Qualification Tests: Qualification
test , or preproduction tests, shall be run by Itek
in Boston on a complete camera subsystem, to demonstrate compliance with the
subsystem performance requirements. The individual tests shall be run with
no adjustments or repairs during the course of the test. If any modifications
are necessary after the completion of any qualification test, the test must
Approved For
~1&99ftfty!T_
UOQ728R00 300070003-7 4 9 8 4 9
Shcer 15 of 25 Sht ors
 nM!lL)LING
Approved or Release : CIA-RDP66B00728R000300070003-7
4.3.1.2.2 Test levels and limitation shall be as
follows:
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS 4 9 8 4 9
Approved For elease 2001/04/20 : CIA-RDP66B007728R00 -
SPECIAL i"74 -1A1DLING Sheet 16 of 25 Sheets
be re-run, unless explicit waiver is granted upon demonstration that the
modification will not affect the response to the particular test. The camera
shall be qualified under the applicable portions of 6117, using environments
specified for the "Payload Area".
4.2.1.2 Subassembly Qualification: Subassemblies of the
Strip Camera subsystem shall be separately qualified
under the applicable portions of 6117, using environments specified for
Payload Area. Subassemblies need not be given qualification tests if prior
qualification under test conditions at least as severe as required in this
specification can be documented or if waiver is granted by SE/TD upon review.
Specific acceptance must be granted by SE/TD for each subassembly not
subjected to qualification. Parts must function correctly following exposure
to qualification test requirements.
4.2.2 Acceptance Tests: Acceptance tests shall be run on production
units to verify workmanship and operability. The individual
tests shall be run with no adjustments or repairs during the course of the
test. If any modifications or repairs are made following the completion of
any acceptance test, all tests previously run on the unit must be repeated,
unless an explicit waiver is granted by SE/TD, based on the demonstration
that the modification or repair will not affect the response to the particular
test or tests.
4.3 Qualification Test: The environments specified in 6117 are for
ascent and on-orbit. After simulated ascent environment, satis-
factory camera operation must be demonstrated. The shock in paragraph 4.3.2.1.2
is applicable to the cassette subassembly for recovery environment after which
operation is not required but disassembly will be demonstrated. (See paragraph
3.9.4.1.)
4.3.1 Camera Subsystem Qualification Tests
4.3.1.1 Shock Test: The camera subassemblies shall
operate after being subjected to the required
shocks. Operating during shock is not required. The provisions of paragraph
4.9 of 6117 are applicable. Table III, Payload (preliminary) test conditions
shall apply.
4.3.1.2 Vibration Test: The camera shall operate after
being subjected to the required vibrations. Operation
curing vibration is not required. The provisions of paragraph 4.10 of 6117
shall apply and Table V with be following modifications.
4.3.1.2.1 White noise testing is not required.
 400-3000
7.5 g
lete Unit
Com
X
15-400
1.5 g
p
400-2000
3.0 g
Y,Z
15-400
1.0 g
400-2000
3.0 g
U
d
Z
Y
X
-2000
20-2000
.25 to .Sg
Unit an
,
,
15 min down
in u
15
a Lens only
u
p,
m
i
c
Minor Assemblies
Elec. and Mech.
Major Subassembly
Optical Bar
F' Transport
o Spool & Drive
a Cassette
u
w
AXES
LEVELS
(30 min, Log Sweep
each axis)
X,Y,Z
5-20cps
.5" D.A.
20-1500
10 g
1500-3000
15 g
X
5-12cps
.5" D.A.
12-400
4 g
400-3000
7.5 g
Y ,z
5-9cps
.5" D.A.
9-250
2 g
250-400
4 g
400-3000
7.5 g
STM X,Y,Z 5-9cps .5" D.A.
0 9-250 2 g
a' 250-400 4 g
d H
1) All "g" values are 0 to peak.
2) Resonances at' frequencies other than those in
the range from 15-25 cps shall be monitored
and used to limit
willtnot beeexshaker ceededso
that above "g"
Resonances in the 15-25 cps range shall subject
the equipment to design review.
4.3.1.3 Thermal Altitude: An endurance run, corresponding
in duration to the mission duration shall be run,
SPECIFICATION FOR STEREU 5-1Kr
oINDEX CAMERAS
Approved For Reloase
"I/U4/20 : CIA-RDP66B00728R0003
SPECIAL
 Approlged Fa
at'simulated altitude, and internal thermal environment specified. The
duration of the test shall be 96 hours. The operation of the equipment will
approximate the normal duty cycle. The test shall be run using a simulated
vehicle power supply. No adjustments shall be made during the test. Loss of
altitude during the test, to pressures greater than 0.001 mm Hg shall invalidate
the test. At least 48 hours of the normal duty cycle during this test shall
be at maximum cycling speed. The test shall be run at a pressure of less than
0.0001 millimeters mercury absolute pressure. The equipment shall be mounted
in vehicle fairing, and jig-type take-up cassette used. The temperature shall
be maintained at 70 + 10 degrees F for the duration of the test.
4.3.1.4 Voltage Sensitivity: Tests shall be run at high-
and low-input voltages, with noise and ripple
up to 2.0 volts peak-to-peak at 2000 cps on the power supply. The equipment
shall be operated at atmospheric conditions, at both maximum and minimum cycling
rates over the range of operating voltages specified in this specification.
4.3.1.5 Acceleration Tests: The camera shall operate after
being subjected to the required accelerations.
Operation during the acceleration phase is not required.
4,3.1.6 Optical Resolution: The camera shall meet the
optical resolution requirements of this specification
as stated in paragraph 3.8.1 of this specification. Thaeoptical resolution
shall be measured at vacuum conditions. This test shall be run after the
completion of all other tests.
4.3.1.7 Temperature Tests: The following tests will be
accomplished to establish equipment operating
capabilities at predicted extremes of temperature. It is recognized that
subsystem performance parameters may be degraded since these temperatures are
beyond normal operational design limits:
4.3.1.7.1 High Temperatures: The camera shall be
operated after stabilization at high
temperature. The equipment shall be operated at a temperature of 95 + 5 - 0
degrees.F at a pressure of 0.001 mm mercury absolute for at least 5 minutes
each at minimum and maximum cycling rates.
4,3.1.7.2 Low Temperature: The camera shall be
operated after stabilization at low
temperature. The equipment shall be operated at a temperature of 45 -5 +0
degrees F at a pressure of 0.001 mm mercury absolute for at least 100 cycles
each at minimum and maximum cycling rates.
4.3.2 Subassembly Qualifications: Strip camera subsystem
subassemblies shall be subjected to all tests called for in
Approved For R
TITLE
SPECIFICATION FOR CSATEERREEOOSSTRIP
seST1~UT104/~1ER-RDP66600728R000
SPECLU
00070003-7 4 9 8 4 9
 ,,. , batU HANDLING
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
Camera Subsystem Qualification Tests as outlined. However, alternate versions
of the Thermal Altitude endurance run may be substituted where applicable.
4.3.2.1.1 Ascent Shock: The camera subassemblies
shall operate after being subjected to
the required shocks. Operation during shock is not required. The provisions
of paragraph 4.9 of 6117 are applicable. Table III, Payload (preliminary)
test conditions shall apply.
4.3.2.1.2 Recovery Shock: The cassette shall be
capable of withstanding the following
shock test with a full spool of film without damage to the film nor degradation
of the information recorded thereon. It shall be capable, furthermore, of
withstanding said shocks without structural alteration which would cause
damage to the film or degradation of the recorded information during subsequent
disassembly of the cassette. Subject the cassette to 3 shocks along each
direction of both X and Y axes for a total of 12 shocks of 5g magnitude and 6
millisecond duration (half sine pulse). Subject the cassette to 20 g's for
3 shocks in each direction along X axis. Axes defined in 49090.
4.3.2.2 Altitude: The equipment shall be operated at a
pressure of less than 0.0001 mm mercury absolute
pressure, for a normal four-day mission.
4.3.2.3 Voltage Sensitivity: The equipment shall be
operated at atmospheric conditions at high and
.low voltages required in psvagraph 4.3.1.4.
4.3.2.4. Temperature Tests: The following tests will be
accomplished to establish equipment operating
capabilities at predicted extremes of temperature. It is recognized that
subsystem performance parameters may be degraded since these temperatures
are beyond normal operational design limits.
4.3.2.4.1 High Temperature: The equipment shall
be operated at a temperature of 90 +5 -0
degrees F at a pressure of 0.0001 mm mercury absolute for 30 minutes.
4.3.2.4.2 Low Temperature: The equipment shall
be operated at a temperature of 45 +0 -5
degrees F at a pressure of 0.0001 mm mercury absolute for 30 minutes.
4.3.2.5 Electronic Package High and Low Temperatures:
Electronic packages shall be run for 30 minutes
under simulated load and mounting, after stabilization at a pressure of
0.001 mm mercury absolute at 125 + 5 degrees F. They shall also be
subjected to the same test conditions except temperature stabilization shall
be 40 +0 -5 degrees F.
Approved Ford
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS
Release 2001/04/20: CIA-RDP66B00728R0
SPECLA:L HANDLING
4 9 8 4 9
0300070003 7
Sheets of 25 Sheets
 Approvea
4,3.2.6 Vibration Test: The subassemblies shall operate
after being subjected to the required vibrations.
Operating during vibration is not required. The provisions of paragraph 4.10
of 6117 shall apply and Table V with the following modifications: White noise
testing is not required. Test levels and limitations to be those in 4.3,1.2.1.
4,4 Acceptance Test Requirements
The camera shall be subjected to the following tests.
4.4.1 Electrical Insulation Tests: All electrical circuits shall
be checked to the frame of the camera with a single
application of 100 volts DC on 28-volt circuits and 300 volts DC on 115-volt
circuits, and shall show a resistance of 1 megohm or greater. The wire
harness shall have been tested to the limits of 1072045 after installation
in the camera but prior to connection of subassemblies and components.
4.4.2 Mating and Alignment Test: The camera will be mated to a
test fixture simulating the mechanical interfaces per
This test.fixture will be a precision instrument and the camera must fit the
interface without alteration of the fixture. The camera subsystem must align
on all axes in accordance with this specification. Position of the camera
alignment marks shall be checked with respect to the optical axis. These
marks shall coincide with the optical axis within 15 minutes of arc and any
misalignment shall be known to within 3 minutes of arc and recorded. Load
the camera with a full spool of test film to be used in all succeeding tests.
4.4.3 Functional Operation Test: With the simulated electrical
interface of the Checkout Console the camera will operate
satisfactorily,and respond to all operational and test commands. The camera
will be operated at the'extreme ends of mid-point of the V/h range, The
camera shall be loaded with film and operated in conjunction with an actual
take-up cassette in a positioning fixture. The camera shall operate
satisfactorily for 1000 feet of film without an assist of any manner whatsoever.
The camera shall, be started and stopped at least twenty-five times without
any erratic operation or mishandling of film. Any malfunction of loops,
tracking or dancer rollers may be corrected but the complete test shall be
re-run,
4.4.4 Power and TM Test: With the subsystem connected to the
L simulated electrical interface of the Checkout Consoles,
a test shall be conducted to determine that subsystem circuits do not exceed
the power requirements. Power and signal checks shall be made at designated
connector pins of the Electrical Interface, Real time recordings of
functional TM instrumentation at high and low ramp settings will be obtained
to demonstrate satisfactory operation. Single point thermal instrumentation
calibration will be accomplished. Three point data on serialized thermal
Approved For
TITLE
SPECIFICATION FOR STEREO STRIP
Reease MAW G MK6B00728R0 0300070003-7 4 9 8 4 9
 SPECIAL HANDLING
Approved or Release - -
4.4.5 Vibration Test: The Strip Subsystem mounted on the test
fixture shall be placed on a vibration table. Voltage will
be applied at J101 per SP2-156 during vibration but the unit will not be
operated. Sinusoidal vibration shall be applied along each of three mutually
perpendicular axes, at 1/2 to 1 g peak-to-peak using a frequency sweep program
from 20 to 2000 cps at constant octave sweep rate for 15 minutes, followed by
a sweep from 2000 to 20 cps at constant octave sweep rate for 15 minutes.
Resonances will be monitored and used to limit the input of the shaker to the
levels specified herein. Dwell at resonance is not required.
4.4.6 Post-Vibration Visual Inspection: After the vibration teat,
the subsystem shall be inspected for any visual defects.
4.4.7 Post-Vibration Electrical Insulation Test: After the
vibration test, all electrical circuits shall be checked
to the frame of the camera with a single application of 100 volts DC on
28-volt circuits and 300 volts DC on 115-volt circuits, and shall show a
resistance of 1 megohm or greater.
4.4.8
Post-Vibration Operating Test: After vibration test the
3.3. above.
subsystem shall be operated in accordance with paragraph
4.4.9
Post-Vibration Photo Test
4.4.9.1 Resolution: The camera shall be mounted in the
dynamic resolution tester, loaded with a test spool
of unexposed SO-132 film and vacuum conditions less than 500 microns shall be
obtained.. The camera shall operate and photograph the test patterns under
dyne~tt onditions, to demonstrate satisfactory operation and perform
resolution tests in accordance with this specification. Using the resolution
target (per para. 3,8.1), with the camera running at nominal V/h and minimum
operational slit for SO-132, set DRT light source level for optimum exposure.
Make three exposures on axis at each of the following field angles: 00, + 10,
+ 20 for a total of 5 angular positions. Process the film under controlled
conditions and record gamma. Read the three target images in accordance with
MIL-STD-150A recording the average of the two highest readings. Calculate
and record LWAR.
L
4.4.9.2 Format Banding and Light Tightness: A fogging test
of live film shall be administered to demonstrate
light tightness of the subsystem using a simulated structure. The fogged
film shall be inspected to ascertain that format dimensions are within the
design accuracy required. Banding shallbe shown to produce less than 0.15
Approved For
TITLE
SPECIFItATION FOR STEREO STRIP
Id 8R0 300070003-7 4 9 8 4 9
ea3f~D1XC-6B007`2~.
SPEC' ir4m ~~a~., ~1.7
CF or 91 -f:74 c.
 ?TM ? SPECIAL H
Log E change. Determine delta Log E by reference to the straight line portion
of 80-132 sensitometric control film printed and normally processed under
controlled conditions recording gamma.
5.0 PREPARATION FOR DELIVERY
5.1 Packing and Packaging: Packing and packaging shall be adequate
to protect all equipment when shipped or stored.
5.2 Handling, Mating and Checkout: Adequate protective devices
will be supplied.
TITLE,
SPECIFICATION FOR STEREO STRIP
Approved For R fs~Hb/I1tDE8IB00728R000 00070003-7 4 9 8 4 9
C, D C! /+. 8 f ,?' ,, ; ' 1 1 i (-I 22 - r --or
 ~-- p ve or a ease 26-01/04/20 CIA-RDP66B00728R000300070003-7
Exceptions to 2.0 APPLICABLE DOCUMENTS
h. Change paragraph 4.1_1 to read "humidity of not more than 70
percent."
i. Paragraphs 403 through 4.8.3 - not applicable.
J. Delete paragraph 4.9.1 and 4.9.2.
k. Delete paragraph 4.10_1.
1. Table VI - not applicable.
m, Paragraph 4.10.2 will be used as a guide in preparing the
Qualification Test Specification, Procedures, and design of the
qualification fixtures.
TITLE
SPECIFICATION FOR STEREO STRIP AND
S`tBLLAR/INDEX CAMERA SUBSYSTEMS 49849
Approved For R?Iease 2001/04/20 : CIA-RDP66B0^00728R000 0O3=?25 0O3=?SPECIAL S1lc?~_'t 23 `i 25 Sfit'i'(.S
c .7_
f. Delete paragraph 2.4.
1.0 Exceptions to 61178:
a. Change paragraph 101.5 to read "AET Engineering Department of
Contractor."
b. Delete paragraph 1.2.2.1 and substitute "Equipment shall be
transported by military transport aircraft and motor vans.
The equipment shall be protected and packaged to withstand
such conditions as well as shock and vibration prevalent
during shipping."
c. Delete paragraph 1.2.3 and substitute "Contractor storage
facilities will ordinarily be air-conditioned. However, heat
and high humidity may occur, and equipment should be able to
withstand such conditions."
d. Delete paragraphs 1.2.4.1, 3.2.1.4, 3.2.1.5, 4.3.1, 4.4, 4.6,
4.7, and 4.8.
eo Change paragraph 2.1 to (ASG)-13alApTestril
and Amendment No.. 1, 20 J n ry Aeronautical and Associated Equipment, General Specification
for":- all other MIL standards not applicable.
g. Delete paragraphs 3.2,1, 3.2.2.2, and 3.2.2.3.
 Approved for a ea 8R000300070003-7
2.0 Exceptions to 447969A:
2,1 The following techniques, which have proved effective in the past
will be employed for grounding and shielding and will satisfy the
general intent of 447969A and the requirements of this Specification.
2.1.1 The chassis will in no case be used as a circuit path.
There will be a minimum isolation of 1 megohm between
chassis and all power and signal circuits.
2.1.2 Loads on each power category will be kept separated
throughout the camerae That is, regulated return,
unregulated return, 400-cycle return and TM return will not tie to each
other in the camera.
2.1.3 No attempt will be made to float electronic chassis
with respect to the structure.
2.1.4 Each electronic chassis will be tied electrically to
a central chassis ground point.
2.1.5 All 400-cycle circuits will be run twisted shielded.
2,106 All 'shields at the interface, if picked upin the camera,
',will, be carried through Interface connectors to the load
or signal source.without comuoning to other shield circuits and without being
tied to any pour return circuit or chassis.
2.1.7 :Connector pins will be allocated to maintain spacing
between power and signal circuits.`
2.1.8 Shields will be'grounded at but a single point. Shields
.,will be insulated from each other in cable bundles.
2.1.9 Power distribution to subsystems not essential to the
primary flight objective will be fused. .
2.1.10 Wire sizes will be selected consistent with MIL-W-8160C.
2.1.11 Radio interference criteria will be applied for the entire
camera rather than on a component or subassembly basis.
TITLE
SPECIFICATION FOR STEREO STRIP AND
00300070003-7
Approved Fo~ffeVa-se'Z001/v4 CIA$RDP6M728R0
SPEC[ ~,~:. DLING,
shc'e t 24 of 25 sh.tts
 SPECIAL HANDL:IN
2.1.12 The overall schematic will show the shields and grounds
distribution details.
2.1.13 The following techniques will be employed in the camera
to reduce radio interference at its source.
2.1.13.1 Dual LC filters will be used in conjunction
with all DC motors.
2.1.13.2 Diodes or arc suppressors will be used to
reduce inductive transients on relay coils,
brakes, and solenoids.
2.1.13.3 Mounts for motors, etc., are spot-faced to
provide good contact with the frame. '
TITLE
SPECIFICATION FOR STEREO STRIP
AND STELLAR/INDEX CAMERAS
Approved For elease 2001/04/20 :~ CIA-RDP66B00728R00 300070003-7 4 9 8 4 9
 Approved For ReleasSPRI 22 : RpUUMPR000300070003-7
Model Unit
Cost Summary
Materials
Strip Unit - Electrical/Mechanical
Cost Summary
~OG
&K-a-97-
COPY or
Materials
9
Strip Unit - Optical
10
Cost Summary
11
Materials
12
Optical Test Equipment
13
Cost Summary
14
Materials
15
Strip DIRT
16
Cost Summary
17
Materials
Ground Support & Handling Equipment
18
19
Cost Summary
20
Materials
21
Test Program
22
Cost Summary
23
Materials
24
Program
25
Cost Summary
26
Materials
27
Travel Schedule
28
Communications
28
Security
29
Palo Alto Support
30
Cost Summary
z
31
Materials
DOCUMENT NO.
-
unications
C
NO CHARGE I'M CLASS. 0
31
omm
^ DECLASSIF12D
32
Travel Schedule
CLASS. CHkI C I.: TO
KLXT R. ~ ~~f ~;.Tnl
TS
Labor Rate Schedule
Funding Forecast
AIi1 H: HR 14.2
DATIit 17-7- ~' REYIEWeRt-000632.
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
SPECIAL HANDLING
 25X1A
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 Page 2 of 34 Pages
Approved For Release 2001/&IRECIA&J NDUNG0070003-7
BOSTON
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 Page 3 of 34 Pages
Approved For Release 20011 DC~ - D WQQ 00070003-7
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
Cocci M HANDLING
 25X1A
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 Page 6 of 34 Pages
Approved For Release 2001/SPECIAL HAnIDth I600070003-7
STRIP UNIT - ELECTRICAL/MECHANICAL
Approved For Release 2001/04/20 : CIA-RDP66B00728R000300070003-7
SPECIAL HANDLING
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 Page 9 of 34 Pages
Approved For Release 2001/913EGIAt-DF QND0070003-7
STRIP UNIT - OPTICAL
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SPECIAL HANDUNG-i
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 Page 12 of 34 Pages
Approved For Release 2001/%ECqAgD tQM jM0070003-7
OPTICAL TEST EQUIPMENT
Approved For Release~Q,Q~,/q,~2Q
? LCI~4;F~D MT. N 6000300070003-7
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 Page 15 of 34 Pages
Approved For Release 200' "tjCi4-R$gWf$5t$F O00070003-7
STRIP DRT
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 25X1A
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 Page 21 Hof 14 Pages
Approved For Release 200Cg:1Rrf4MG300070003-7
TEST PROGRAM
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cDFCaMw WA NW
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PROGRAM
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SPECIAL HANDLING
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 Page 29 of 34 Pages
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SPECIAL HANDLING
PALO ALTO SUPPORT
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 25X1A
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