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DIFFRACTION GRATINGS OF DIRECT IMAGE VIEWER FINAL REPORT PHASE II TRIAL #1(Sanitized)

Document Type: 
CREST [1]
Collection: 
NGA Records (Formerly NIMA) [2]
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP78B04747A001700010013-9
Release Decision: 
RIPPUB
Original Classification: 
K
Document Page Count: 
16
Document Creation Date: 
December 28, 2016
Document Release Date: 
April 25, 2001
Sequence Number: 
13
Case Number: 
Content Type: 
REPORT
File: 
AttachmentSize
PDF icon CIA-RDP78B04747A001700010013-9.pdf [3]1.68 MB
Body: 
DIFFRACTION GRATINGS FOR DIRECT [MAGE VIEWER Final Report Phase II Trial #1 STATOTHR Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 DIFFRACTION GRATINGS for DIRECT IMAGE VIEWER Report on Phase II Trial #1 STATOTHR Declass Review by NIMA/DOD Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 tinerV Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 1.0 The Diamond Tool A fixture was designed and built for generating the short radius diamond tools required. (Photo included). Two diamond tools were made and were checked for radius and true arc, using a microscope with eyepiece scales specially made for this purpose. Each tool has two edges, and the four possible radii were measured and found to be in the range of 76 to 93 microns. 2.0 The Ruling Set Up Several grating blanks were suitably coated with aluminum and all in the same run. Test grooves and test areas were ruled under various conditions of tool orientation and loading. Ruling and overruling was performed with various ruling depths for each pass. 2.1 Set Up Control An interference microscope was used visually and photographically to find the best combination of tool orientation and loading, and to find the best combination of tool loadings for double ruling. Three micro-interferograms were measured for precise groove shape and the result plotted graphically. The first was of a single groove and was used to check the groove contour without the cross effects of adjacent - 1 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 grooves. The second was of adjacent grooves fully ruled in one pass, and clearly shows the unsymmetrical distortion caused by adjacent ruling, The third was of adjacent grooves ruled in two passes, and shows the considerable improvement in groove contour obtained by double ruling. Interferograms and graphs are included in this report. 3.0 Ruling and Replication STATOTHR A master ruling was made, using the double ruling technique. The ruled area is 53 x 53mm and on a 58 x 58mm blank. Two transmission replicas of this ruling were made on blanks 58 x 58 x 10mm. The blank material is fine annealed BSC-2 glass. 4.0 Grating_ Tests The distribution of energy among the orders of the transmission replicas was measured, and for six dis- crete wavelengths in steps of 10m, between 500 and and 550 m?. The results were plotted on a bar graph. 4.1 Test 4.0 was simulated numerically and computed, assuming a theoretically correct groove shape. Results were plotted on a bar graph for comparison to 4.0. - 2 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 4.2 Test 4.0 was simulated numerically and computed using the actual groove contour as plotted graphically from a micro-interferogram. The first computation was found to be inadequate in that the cubic least square fit used in deriving the groove shape coordinates was not close enough to the actual contour. 4.2.1 It thus became necessary to read manually 100 coordi- nates from the plotted groove contour, in order to derive computed energy distribution that could be compared in a meaningful way with the actual energy distribution. The time required to go through this additional work made it impossible to include the result in this report. 5.0 Test Results The micro-interferograms have effective magnifica- tions of 1050x across the groove and 14,500x for the depth of the groove. As plotted graphically, the magnification is approximately 10,000X and 100,000X respectively. The graphs also include a curve which is a true arc calculated from the measured width and depth of the groove. The departure of the groove pro- file from the true arc is 0.05 microns for a single groove, 0.26 microns for single ruled adjacent grooves, and 0.087-microns (3.4 micro inches) for double ruled adjacent grooves. The great advantage of - 3 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 double ruling is thus graphically illustrated. 5.1 The measured energy distribution among the orders for transmission grating #970 was examined for variation of the important ratios between them. For discrete wavelengths, 520m? is the best choice with an overall maximum ratio of 6.4 to 1, between lowest and highest order, and 3.1 to 1, the greatest ratio between adjacent orders. However, when the entire wavelength region, 500 to 550m?, is integrated and at the same time modified by the energy curve for a tungsten source and the spectral response of the eye, the overall effec- tive ratio becomes 4.7 to 1, and 2.9 to 1 for adjacent orders. This comes fairly close to meeting the require- ments of this grating. 5.1.1 It is quite evident from these graphs that even relatively small changes in wavelength have con- siderable influence on the nature of energy distri- bution amongst orders. One can also see that a suitable mixture or range of wavelengths, rather than a single narrow band, is capable of improving the uniform energy distribution problem. 5.2 By way of comparison, and for discrete wavelengths, the choice of wavelength for a theoretically perfect groove shape is also 520m?, in which case the maximum - 4 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 overall intensity ratio is 1.9 to 1, and 1.7 to 1 for adjacent orders, This proves that the effect of wavelength, first noted experimentally, is con- firmed by theory. - 5 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11: CIA-RDP78604747A001700010013-9 6.0 Conclusions and Recommendations The test rulings herein described approach the theoretical distribution of energy, and should provide the means to some useful visual experiments that will tell how good the energy distribution has to be. More meaningful specifications can then be written. We can now see our way to three (3) possible ways of improving on the present test ruling. The first would be to triple rule instead of double rule. However, this would only lead us a little closer to the theo- retical distribution, which at present appears to be barely acceptable. The second way would be to alternate the ruling. We would rule every other groove and then rerule to fill in the spaces. This would lead to symmetrical grooves, but probably alternate grooves would differ in actual shape even if we were to double rule the alternate ruling. And again, we would only be approaching the uneven theoretical distribution of energy in the orders except with somewhat improved symmetry. The third way would be to rule grooves twice as large. We would then have two orders everywhere we now have one order. This overlapping of orders should average the energy in the orders in use, namely, every other order. This third method seems the most promising to - 6 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11: CIA-RDP78604747A001700010013-9 us in that we would be improving on the theoretical possibilities rather than merely trying to approach a less than perfect theoretical solution. On the negative side, the third method does introduce new problems. We would have to form grooves twice as large, necessitating reforming of much more material. Also, we should go back to Phase I type computation first to prove the theory of the energy distribution in the overlapping orders. Since the tool radius required will be roughly twice as large, a new set of tools will have to be made introducing a delay of one month. Nevertheless, it appears that Method 3 is the one most worthwhile to follow in Phase lib of this project. The following are appended to this report: 1. Photograph of diamond tool generating fixture 2. Micro-interferograms of groove profile 3. Graphs plotted from micro-interferograms /1., Bar Graph-Measured order intensities for discrete wavelengths 5. Bar Graph-Calculated order intensities for discrete wavelengths 6. Bar Graph-Relative order intensity for given source, receiver and band pass, derived from measured intensities. 7. Bar Graph-Calculated order intensities for discrete wavelengths derived from measured groove contour (Fig. 2). - 7 - Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Diamond Lapping Fixture For generating short radius tools Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Approved For Release 2001/05/11 : CIA-RDP78604747A001700010013-9 Micro-Interferogramls of groove contour Magnification: 1050X Fori7ontal 14500X Depth Micro-Interferogram of a single groove. 7 1/2 fringes (in oil) deep and 33.4 microns wide. Micro -Interferopram of two adjacent grooves ruled in one pass. 10 fringes (in oil) deep and 36.2 ocrons wide Micro-Interferograrr of tw cent grooves ruled in two 9 fringes (in oil) deep a microns wide. adja 'passes. nd 36.2 or Release 2001/05/11: CIA-RDP78604747A001700010013-9 ease 2001/05/11 : CIA-RDP78B04747A001700 CONTRACT . DATA PLOTTED FROM MICRO-INTERFEROGRAMS SOLID LINE - Radius calculated from width & depth of groove. DASH LINE - Measured groove contour for leading side of groove. 'DOTTED LINE Measured groove contour for trailing side of groove. Ruling: 111001111010111111111111111ffillffilint IN liii IUNHIIIIIIHIIIHIHIHIIIIHIHIHIIIIIII INIONOMMIIIMMEilho WIRMIRONIIN omummummilogro IIIIIIIU lihIllllllhIIllhIIIIllI011hIIllINllllIUll IIIHHIIjHJ Napo4I NIH opponifi Emil mom mu ii moommomploommio ommumuuddlifininundo ifiummoomm immiummomirmw mourpopp imo cisismidffidi llm 1111 11.1 111 it II:1 IL Ft 1 1 Ii 1. h ,I III 1111 STATOTHR J i i A ihw?ui IN 11111111110011 A h gm mom RN imilla MEE MIMEO I JAM I iffinffillii? 1 low 0 muslmouffigemill 11. AINIMMINilin Mifilli 111111111111011111 r gi MINIM I I,IIIW III mimmourimmi II WINO air 11 1 111111151 r lom i mmompoim Joon iimummmi PAN1114111. Mill11111111111WAINE n 111511111111111111in Wm ? (I 111111 41111119rIll I ? " 111111"Er Nu e 1 III r 1,15,11111111JAY? SINGLE GROOVE Radius= 85 u V III 1 II milIUMIUUMOHOMI Oififfill iffilliMMUNIMilpill IIIMUMMUMMUMMINJUI IMMO I 1111111111M010111011111NOPM i rimmummulluommoommummum 01111110111111111111111111111111111111111111M11111 1 IMMIIIMMEMIHUMM11111111 1111 EMUMMEIMIIIMIMMINImil m MIME moon= wo in MEM MUMMUTIOU MH UN PIPAIRMIll, pm mpiiP, mommem mn Plgsa 6 linallilli iiiii 1 oummr simu Norm umumnreirmomm ti Itil 11 i 4 41- ? i; 1 1' 1-11 titii ADJACENT GROOVES SINGLE RULED Radius = 75 u iii it 41-i 11' I OW6 MOMMIN111 EllimEMMIN MI - IMMO nom Nom u.. II I I 1 II 1 till 61'1 Ii ADJACENT GROOVES DOUBLE RULED Radiui ='83.5 u SCALE 1 It' II mum I MOM m.1 111 ILI ii 44 minuo ill 11 Id ME II MIME MM011 MPH INllhIOOl1I kil I .1 011111 1 'iOIIIIIIIIIIIIIHiOHIHIIHUHIIIIIIIOIHIWNIIIIIIIOII WirilimiliMINE Li NE 1 111111 Flit III11110IIIIIIIIIIIIIHIIIIIIIII1IHOIIOIIIIHIIIIIIIIIIOIIOI iffillffilll1111110elifiliMENEMINWHIMIIINifi0 IIIOIHIHIHNIIIOIIHIOHI1OIIIOHIIHIIIIIIIIIOIOO PRTIIMPRIIIMMIMMOIMMIUMIONIMUMNI IMPANUOUUMUIMIUMMUIUMIUM Approved For Release 2001/05/11 CIA-RDP78B04747A0017000100/4-9 10 /2 efe ease 2001/05/11 : CIA-RDP78B04747A001700 CONTRACT . DATA PLOTTED FROM MICRO-INTERFEROGRAMS SOLID LINE - Radius calculated from width & depth of groove. DASH LINE - Measured groove contour for leading side of groove. 'DOTTED LINE Measured groove contour for trailing side of groove. Ruling: 111001111010111111111111111ffillffilint IN liii IUNHIIIIIIHIIIHIHIHIIIIHIHIHIIIIIII INIONOMMIIIMMEilho WIRMIRONIIN omummummilogro IIIIIIIU lihIllllllhIIllhIIIIllI011hIIllINllllIUll IIIHHIIjHJ Napo4I NIH opponifi Emil mom mu ii moommomploommio ommumuuddlifininundo ifiummoomm immiummomirmw mourpopp imo cisismidffidi llm 1111 11.1 111 it II:1 IL Ft 1 1 Ii 1. h ,I III 1111 STATOTHR J i i A ihw?ui IN 11111111110011 A h gm mom RN imilla MEE MIMEO I JAM I iffinffillii? 1 low 0 muslmouffigemill 11. AINIMMINilin Mifilli 111111111111011111 r gi MINIM I I,IIIW III mimmourimmi II WINO air 11 1 111111151 r lom i mmompoim Joon iimummmi PAN1114111. Mill11111111111WAINE n 111511111111111111in Wm ? (I 111111 41111119rIll I ? " 111111"Er Nu e 1 III r 1,15,11111111JAY? SINGLE GROOVE Radius= 85 u V III 1 II milIUMIUUMOHOMI Oififfill iffilliMMUNIMilpill IIIMUMMUMMUMMINJUI IMMO I 1111111111M010111011111NOPM i rimmummulluommoommummum 01111110111111111111111111111111111111111111M11111 1 IMMIIIMMEMIHUMM11111111 1111 EMUMMEIMIIIMIMMINImil m MIME moon= wo in MEM MUMMUTIOU MH UN PIPAIRMIll, pm mpiiP, mommem mn Plgsa 6 linallilli iiiii 1 oummr simu Norm umumnreirmomm ti Itil 11 i 4 41- ? i; 1 1' 1-11 titii ADJACENT GROOVES SINGLE RULED Radius = 75 u iii it 41-i 11' I OW6 MOMMIN111 EllimEMMIN MI - IMMO nom Nom u.. II I I 1 II 1 till 61'1 Ii ADJACENT GROOVES DOUBLE RULED Radiui ='83.5 u SCALE 1 It' II mum I MOM m.1 111 ILI ii 44 minuo ill 11 Id ME II MIME MM011 MPH INllhIOOl1I kil I .1 011111 1 'iOIIIIIIIIIIIIIHiOHIHIIHUHIIIIIIIOIHIWNIIIIIIIOII WirilimiliMINE Li NE 1 111111 Flit III11110IIIIIIIIIIIIIHIIIIIIIII1IHOIIOIIIIHIIIIIIIIIIOIIOI iffillffilll1111110elifiliMENEMINWHIMIIINifi0 IIIOIHIHIHNIIIOIIHIOHI1OIIIOHIIHIIIIIIIIIOIOO PRTIIMPRIIIMMIMMOIMMIUMIONIMUMNI IMPANUOUUMUIMIUMMUIUMIUM Approved For Release 2001/05/11 CIA-RDP78B04747A0017000100/4-9 10 /2 efe ease 2001/05/11 : CIA-RDP78B04747A001700 CONTRACT . DATA PLOTTED FROM MICRO-INTERFEROGRAMS SOLID LINE - Radius calculated from width & depth of groove. DASH LINE - Measured groove contour for leading side of groove. 'DOTTED LINE Measured groove contour for trailing side of groove. Ruling: 111001111010111111111111111ffillffilint IN liii IUNHIIIIIIHIIIHIHIHIIIIHIHIHIIIIIII INIONOMMIIIMMEilho WIRMIRONIIN omummummilogro IIIIIIIU lihIllllllhIIllhIIIIllI011hIIllINllllIUll IIIHHIIjHJ Napo4I NIH opponifi Emil mom mu ii moommomploommio ommumuuddlifininundo ifiummoomm immiummomirmw mourpopp imo cisismidffidi llm 1111 11.1 111 it II:1 IL Ft 1 1 Ii 1. h ,I III 1111 STATOTHR J i i A ihw?ui IN 11111111110011 A h gm mom RN imilla MEE MIMEO I JAM I iffinffillii? 1 low 0 muslmouffigemill 11. AINIMMINilin Mifilli 111111111111011111 r gi MINIM I I,IIIW III mimmourimmi II WINO air 11 1 111111151 r lom i mmompoim Joon iimummmi PAN1114111. Mill11111111111WAINE n 111511111111111111in Wm ? (I 111111 41111119rIll I ? " 111111"Er Nu e 1 III r 1,15,11111111JAY? SINGLE GROOVE Radius= 85 u V III 1 II milIUMIUUMOHOMI Oififfill iffilliMMUNIMilpill IIIMUMMUMMUMMINJUI IMMO I 1111111111M010111011111NOPM i rimmummulluommoommummum 01111110111111111111111111111111111111111111M11111 1 IMMIIIMMEMIHUMM11111111 1111 EMUMMEIMIIIMIMMINImil m MIME moon= wo in MEM MUMMUTIOU MH UN PIPAIRMIll, pm mpiiP, mommem mn Plgsa 6 linallilli iiiii 1 oummr simu Norm umumnreirmomm ti Itil 11 i 4 41- ? i; 1 1' 1-11 titii ADJACENT GROOVES SINGLE RULED Radius = 75 u iii it 41-i 11' I OW6 MOMMIN111 EllimEMMIN MI - IMMO nom Nom u.. II I I 1 II 1 till 61'1 Ii ADJACENT GROOVES DOUBLE RULED Radiui ='83.5 u SCALE 1 It' II mum I MOM m.1 111 ILI ii 44 minuo ill 11 Id ME II MIME MM011 MPH INllhIOOl1I kil I .1 011111 1 'iOIIIIIIIIIIIIIHiOHIHIIHUHIIIIIIIOIHIWNIIIIIIIOII WirilimiliMINE Li NE 1 111111 Flit III11110IIIIIIIIIIIIIHIIIIIIIII1IHOIIOIIIIHIIIIIIIIIIOIIOI iffillffilll1111110elifiliMENEMINWHIMIIINifi0 IIIOIHIHIHNIIIOIIHIOHI1OIIIOHIIHIIIIIIIIIOIOO PRTIIMPRIIIMMIMMOIMMIUMIONIMUMNI IMPANUOUUMUIMIUMMUIUMIUM Approved For Release 2001/05/11 CIA-RDP78B04747A0017000100/4-9 10 /2 efe ease 2001/05/11 : CIA-RDP78B04747A001700 CONTRACT . DATA PLOTTED FROM MICRO-INTERFEROGRAMS SOLID LINE - Radius calculated from width & depth of groove. DASH LINE - Measured groove contour for leading side of groove. 'DOTTED LINE Measured groove contour for trailing side of groove. Ruling: 111001111010111111111111111ffillffilint IN liii IUNHIIIIIIHIIIHIHIHIIIIHIHIHIIIIIII INIONOMMIIIMMEilho WIRMIRONIIN omummummilogro IIIIIIIU lihIllllllhIIllhIIIIllI011hIIllINllllIUll IIIHHIIjHJ Napo4I NIH opponifi Emil mom mu ii moommomploommio ommumuuddlifininundo ifiummoomm immiummomirmw mourpopp imo cisismidffidi llm 1111 11.1 111 it II:1 IL Ft 1 1 Ii 1. h ,I III 1111 STATOTHR J i i A ihw?ui IN 11111111110011 A h gm mom RN imilla MEE MIMEO I JAM I iffinffillii? 1 low 0 muslmouffigemill 11. AINIMMINilin Mifilli 111111111111011111 r gi MINIM I I,IIIW III mimmourimmi II WINO air 11 1 111111151 r lom i mmompoim Joon iimummmi PAN1114111. Mill11111111111WAINE n 111511111111111111in Wm ? (I 111111 41111119rIll I ? " 111111"Er Nu e 1 III r 1,15,11111111JAY? SINGLE GROOVE Radius= 85 u V III 1 II milIUMIUUMOHOMI Oififfill iffilliMMUNIMilpill IIIMUMMUMMUMMINJUI IMMO I 1111111111M010111011111NOPM i rimmummulluommoommummum 01111110111111111111111111111111111111111111M11111 1 IMMIIIMMEMIHUMM11111111 1111 EMUMMEIMIIIMIMMINImil m MIME moon= wo in MEM MUMMUTIOU MH UN PIPAIRMIll, pm mpiiP, mommem mn Plgsa 6 linallilli iiiii 1 oummr simu Norm umumnreirmomm ti Itil 11 i 4 41- ? i; 1 1' 1-11 titii ADJACENT GROOVES SINGLE RULED Radius = 75 u iii it 41-i 11' I OW6 MOMMIN111 EllimEMMIN MI - IMMO nom Nom u.. II I I 1 II 1 till 61'1 Ii ADJACENT GROOVES DOUBLE RULED Radiui ='83.5 u SCALE 1 It' II mum I MOM m.1 111 ILI ii 44 minuo ill 11 Id ME II MIME MM011 MPH INllhIOOl1I kil I .1 011111 1 'iOIIIIIIIIIIIIIHiOHIHIIHUHIIIIIIIOIHIWNIIIIIIIOII WirilimiliMINE Li NE 1 111111 Flit III11110IIIIIIIIIIIIIHIIIIIIIII1IHOIIOIIIIHIIIIIIIIIIOIIOI iffillffilll1111110elifiliMENEMINWHIMIIINifi0 IIIOIHIHIHNIIIOIIHIOHI1OIIIOHIIHIIIIIIIIIOIOO PRTIIMPRIIIMMIMMOIMMIUMIONIMUMNI IMPANUOUUMUIMIUMMUIUMIUM Approved For Release 2001/05/11 CIA-RDP78B04747A0017000100/4-9 10 /2 efe /1 1, lox to TO THE 2 INCH 358-12 AiVrvett78-1-81RVF6.1te 2001105/11A-: CIA- P78B04747A001700010013-9 111111171111111.111111111111111 1111.10/11111?111, I I I I I 1111,11/11 -T- .7= ,--------r- jilaill - 4 1 - M IME _ ME =_MIEM- Ellill elliMERN=W2 111111 MIMI la Et..1 I FE ,.., .............. . ,.. r. , mou.winiir .1 lisimiripil :9 E NJ E z LI = DEE IMIIMINIMIEFAINEir mismilmiummimmirlemil --- 1 mum NE 1 IE II NE 1 - , - 1u.- I 0 -Rs ? 88047 A oi 0 01663 ? 771.- Approv 41-For - 17,1 I 4 1/ /6

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