FEASIBILITY OF A POWERED BALLOON AS A HIGH ALTITUDE PLATFORM FOR INTELLIGENCE COLLECTION

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP78-03642A001300040029-2
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
2
Document Creation Date: 
December 22, 2016
Document Release Date: 
June 14, 2012
Sequence Number: 
29
Case Number: 
Publication Date: 
April 14, 1959
Content Type: 
MEMO
File: 
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PDF icon CIA-RDP78-03642A001300040029-2.pdf91.68 KB
Body: 
Declassified in Part - Sanitized Copy Approved for Release 2012/06/14: CIA-RDP78-03642AO01300040029-2 ? CONFIDENTIAL. A- / 14+ April 1959 ) MORANDUM FOR: Assistant Chief/TSS/Research and Development SUBJECT : Feasibility of a Powered Balloon as a High Altitude Platform for Intelligence Collection REEERE1(E : 1. Report Sponso red by "Controllable Balloon Study", 25X1 25X1 2. Report) "Final Report on a Meteorological Study, Sponsored by TSS/ED 3* Memorandum for AC /TSS /R&D from C /TSS /ED dated 28 April 1958 1. Since the date of the memorandum, reference 3 above, considerable study work has been done in an effort to apply predicted powered balloon performance to possible target areas under realistic meteorological con- ditions. Reference 1 was accomplished for a very specific mission, Refer- ence 2 was more general in nature. In both cases the studies suffered from lack of observed data at very high altitudes. 2. From the accumulated studies on powered balloons a feasibility study is presented designed to outline the estimated usefulness of such a vehicle as a platform for intelligence collection devices. In an attempt to make this study stand by itself, some of the estimates previously made have been repeated. Since References 1 and 2 summarize in detail the estimated performance they are referred to in this study. 3. The possibilities for intelligence collection operations using the potential of this vehicle are obviously far from exhausted. It was hoped that complete missions could be run on paper plugging in values for powered balloon performance and upper winds against specific missions. Little hope is now entertained for this idea because of the lack of data on high altitude winds that can be based on actual observations. Wind trajectories in Reference 2 were based on extrapolations of estimates. It is believed that the value of these reports is primarily based on the light they shed on general conditions that can be expected in the areas covered, aircraft. 4+. The feasibility may be briefly summarized by the statement that a powered balloon is the only vehicle now or in the foreseeable future that can remain aloft for extended durations at very high altitudes and under certain conditions can reach targets not accessible by any other CONFIDENTIAL ; / 77 MTV I D00 OEM OAT, aT ORIo COMP' OPI ' ( TYPE _. ORIC CLASS PAGES REV CLASS S..- - JUST _2 IIRXT OEM aSO. _ AUTMi NO i0.2 } Declassified in Part - Sanitized Copy Approved for Release 2012/06/14: CIA-RDP78-03642AO01300040029-2 Declassified in Part - Sanitized Copy Approved for Release 2012/06/14: CIA-RDP78-03642A001300040029-2 CONFIDENTIAL 5. Should an R&D effort be applied toward the establishment of a powered balloon, it is highly recommended that a requirement be levied on the Air Weather Service to take very high altitude weather soundings in areas of possible interest. Further recommendations are: aL.. a. Establish av=MW technical con- sultant on radar shielding methods to follow all phases of design work. Attachment: Feasibility Study: Section I - General Section II - Technical DD/P/TSS/&D~ ~mt Chief TSS/Engineering Division CONFIDENTIAL Declassified in Part - Sanitized Copy Approved for Release 2012/06/14: CIA-RDP78-03642A001300040029-2