RG-72 |
Design Studies and Proposals, compiled 1931 - ca. 1959 |
ARC Identifier: 6408138 |
Former Local Identifier: UD 1044-C |
HMS Record Entry ID: HS1-123390061 |
HMS/MLR Entry Number: P 1044-F |
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Accession Number(s): |
1538 |
2803 |
4461 |
4909 |
6489 |
6903 |
NN3-072-86-002 |
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Declassification Project Numbers: |
NND 55701 |
NND 917657 |
NND 917660 |
NND 917661 |
NND 917662 |
NND 917666 |
NND 927520 |
NND 927521 |
NND 927522 |
NND 927523 |
NND 927531 |
NND 927532 |
NND 927533 |
NND 927534 |
NND 927535 |
NND 927583 |
NND 927584 |
NND 927585 |
NND 927589 |
NND 927591 |
NND 927592 |
NND 927607 |
NND 927608 |
NND 927609 |
NND 927610 |
NND 927611 |
NND 927613 |
NND 927614 |
NND 927615 |
NND 960037 |
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69 Letter Archives Box, Standard |
28 Legal Archives Box, Standard |
1 Log and Printout Box |
1 Flat Storage Box 122 |
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Arranged into two parts. |
Part one is arranged alphabetically by subject and there under alpha-numerically roughly by manufacturer name or design study title. |
Part two is arranged roughly alpha-numerically by manufacturer name or design study title. |
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Brief Box Index: |
Box 1: Design 035 to 120 THRU Vol. 1, Bu Designs D-18, D-23, D-38, D-54A |
Box 2: Vol. 2, Bu Designs D-225, D-228 to D-235, D-239, D-242 to D-244, D-246 to D-250 THRU Vol. 4, Bu Designs D-268 to D-275 |
Box 3: Douglas Aircraft, Model XTB2D-1, Diagrams THRU Chart D: Comparative Sizes of VF Airplanes Fitted with the R1830 Engine Plan |
Box 4: McDonnell Aircraft, F4H-1, Report 5574, Model F4H-1 THRU McDonnell Aircraft, F4H-1, Report 5686-III, Appendix II |
Box 5: McDonnell Aircraft, F4H-1, Report 6346-I, Appendix I THRU OS-130 Day Fighter, Vol. II |
Box 6: Fighter Studies, 1940-1946 THRU Westcoast Engineering Development Corp., Report N-461, Fighter Wing Design Study, Phase I |
Box 7: Westcoast Engineering Development Corp., Report N-471, Fighter Wing Design Study, Phase II THRU Westcoast Engineering Development Corp., Report N-481-3, Wing Structure Investigation Mach 1.3 |
Box 8: Westcoast Engineering Development Corp., Report N-481-4, Wing Structure Investigation Mach 2.0 THRU Boeing Aircraft, Report D-8503, Model 472 Seaplane Design Study, Aerodynamic & Hydrodynamic Analysis |
Box 9: Consolidated Vultee Aircraft, Report ZA-226 THRU Glenn L. Martin Co., P5M-1, Report MER 5087, Martin Model 270 |
Box 10: Glenn L. Martin Co., P5M-1, Report ER 5605 THRU P6M Contract & Planning Files |
Box 11: XP6M-1 Demonstration Requirements for Model XP6M-1 Airplane THRU Test Program Revised XP6M-1 |
Box 12: Navy Department, Research Division, Report DR-1443 THRU XP6M-1 Program Government Furnished Equipment Shortage Status Reports |
Box 13: XP6M-1 Program Change Notices THRU DD 375 XP6M-1 Monthly Progress (Production Program Reports) |
Box 14: XP6M-1 Project Directives THRU Glenn L. Martin Co., XP6M-1, Report 5355 |
Box 15: Glenn L. Martin Co., XP6M-1, Report 5356 THRU W.L. Maxon Corp., Aero X8A Nav. Sys. [Armament Control System (2 copies)] |
Box 16: W.L. Maxon Corp., Improvement in Radar Range Aero X8A Armament Control System THRU Glenn L. Martin Co., XP6M-1, Report ER 4801 |
Box 17: Glenn L. Martin Co., XP6M-1, Report ER 4801 Rev THRU Glenn L. Martin Co., XP6M-1, Report ER 5594, Structural Arrangement Drawing Report |
Box 18: Glenn L. Martin Co., XP6M-1, Report ER 5609, Martin XP6M-1 Substantiation Data Report THRU Martin-Marietta, Martin Engineering Report 7946, YP6M-1 Seamaster |
Box 19: Martin-Marietta, Martin Engineering Report 8781, YP6M-1 Seamaster, Performance Data Substantiation Report THRU Glenn L. Martin Co., YP6M-1, Summary of the YP6M-1 Under Strength 5/58 (5350563 App. 28, 1958) Enclosure I |
Box 20: Glenn L. Martin Co., YP6M-1, Report SER 25 THRU XP6M-1, ER 9086, T-Tail Flutter Model Low-Speed Tests With Revised Fin Stiffness |
Box 21: YP6M-1, P6M-2 THRU Glenn L. Martin Co., XP6M-1, Report ER 7974F, Model XP6M-1, Preliminary Part I |
Box 22: Glenn L. Martin Co., XP6M-1, Report ER 7108, Model XP6M-1 Flight Test Activities Report No. 7 THRU Glenn L. Martin Co., XP6M-1, Report ER 7864, Model XP6M-1 Flight Test Activities Report No. 18 |
Box 23: Glenn L. Martin Co., XP6M-1, Report ER 7868 THRU Glenn L. Martin Co., XP6M-1, Report ER 8395 |
Box 24: Glenn L. Martin Co., XP6M-1, Report ER 8396 THRU Glenn L. Martin Co., P6M-2, Report ER 9322 |
Box 25: Glenn L. Martin Co., YP6M-1, Report ER 9323 THRU Martin-Marietta, Martin Engineering Report 9629 |
Box 26: P6M-1 Procurement Request Forms THRU XP6M-1 Seamaster, Report of Salvage Operations |
Box 27: XP6M-1 Miscellaneous Air Force Information & Requests THRU Glenn L. Martin Co., YP6M-1, Miscellaneous Analysis Data & Drawings (12) |
Box 28: XP6M-1 (Data for Penalties) THRU Lockheed Aircraft, P2V-2, Report 05993, Structural Load Criteria for the 54,000 lb Model P2V Airplane |
Box 29: Lockheed Aircraft, P2V-4, Report 06470 THRU Lockheed Aircraft, P2V-4, Report 07099, Static Test Program |
Box 30: Lockheed Aircraft, P2V-4, Report 07153, Blowout Test of Engine Mount Access Door Diaphragm THRU Lockheed Aircraft, P2V-4, Report 07441, Nacelle Dynamic Loads During Landing |
Box 31: Lockheed Aircraft, P2V-4, Report 07453, PV2-4 Demonstration Landing Gear Tests THRU Lockheed Aircraft, P2V-5, Report 07384, Tension Test of Integral Fitting Extruded Longeron |
Box 32: Lockheed Aircraft, P2V-5, Report 07462, Wing Analysis P2V-5 THRU Lockheed Aircraft, P2V-5, Report 07619, Door Flutter Analysis P2V-5 |
Box 33: Lockheed Aircraft, P2V-5, Report 07620, Preliminary Flutter Analysis Model P2V-5 THRU Lockheed Aircraft, P2V-5, Report 07954, Fuselage Shell Analysis for Skin Thickness Gage Reduction |
Box 34: Zenith Aircraft, P2V-5, Report ZST 40517, Static Test Report-Lac P/N 140074-13 Radome Serial No. 622 THRU Lockheed Aircraft, P2V-5, 6, Report 08660, Static Test Loads P2V-5 & 6 Main Landing gear Ribs |
Box 35: Lockheed Aircraft, P2V-5, Report 08057, Static Test of E.C.M. Operators Ditching Board THRU Lockheed Aircraft, P2V-5, Report 09307, Bow Observers Nose Static Test |
Box 36: Lockheed Aircraft, P2V-5F, Report 10208, P2V-5 Structural Substantiation with Jet Pod Installation THRU Lockheed Aircraft, P2V-6, Report 07629, Structural Analysis of the Model P2V-6 |
Box 37: Lockheed Aircraft, P2V-6, Report 07631, Engine Mount & Nacelle Barrel Analysis THRU Lockheed Aircraft, P2V-6, Report 08597, Structural Analysis of P2V-6 Bat Missile Pylon |
Box 38: Lockheed Aircraft, P2V-6, Report 08598, Structural Analysis of Outer Wing Rework for Petrel & Bat Missile Pylon THRU Lockheed Aircraft, P2V-5, 6, 7, Report 09256, Static Tests of P2V-5, 6, 7 Jet Pod |
Box 39: Lockheed Aircraft, P2V-5, 7, Report 10182, Proof Test of Bomb Support Structure THRU Lockheed Aircraft, P2V-7, Report 08671, P2V-7 Fuselage Structural Analysis Vol. II |
Box 40: Lockheed Aircraft, P2V-7, Report 08672, Model P2V-7 Wing Test & Power Plant Analysis THRU Lockheed Aircraft, P2V-7, Report 08675, Model P2V-7 Landing Gear Analysis |
Box 41: Lockheed Aircraft, P2V-7, Report 08676, P2V-7 Structural Summary & Operating Restrictions THRU Lockheed Aircraft, P2V-7, Report 09786, Proof and Operation Tests of P2V-7 Control System |
Box 42: Lockheed Aircraft, P2V-7, Report 09788, Supplementary Control System Tests THRU Lockheed Aircraft, P2V-7, Report 11349, Summary of Design Data Required for Model P2V-7 (USN |
Box 43: Lockheed Aircraft, P2V-7, Report 11716, Fuselage Shell Analysis Project Julie Modification THRU P2V-7 Airplane Miscellaneous Reports |
Box 44: Grumman Aircraft Engineering Corp., SA-16, Report 2961AF, Detail Specifications for SA-16A Airplane THRU Grumman Aircraft Engineering Corp., Folder 11, XJR2F-1, Aircraft Accident Reports |
Box 45: Temco Aircraft, XASM-N-8, Report 61.036, Structural Air Loads, Rev A 3/20/1959 THRU Temco Aircraft, XASM-N-8, Report 61.154, Fuselage Loads Report, Rev A, Rev B 10/17/1960 |
Box 46: Temco Aircraft, XASM-N-8, Report 61.119, Corvus Quality Progress Report XASM-N-8, 1 July--30 September 1959 THRU Temco Aircraft, XASM-N-8, Report 61.160, Test Plan--Fuselage Structural Test XASM-N-8 |
Box 47: Temco Aircraft, XASM-N-8, Report 61.161, Test Plan--Empennage Tests XASM-N-8 THRU Temco Aircraft, XASM-N-8, Report 61.173, Final Test Report Miscellaneous Tests XASM-N-8 |
Box 48: Temco Aircraft, XASM-N-8, Report 61.174, A4D Pylon Structural Tests XASM-N-8 THRU Temco Aircraft, XASM-N-8, Report 61.528, Test Plan, Low Band Radome Structural Test XASM-N-8 |
Box 49: Temco Aircraft, YASM-N-8, Report 161.92, Flight and Ground Loads Criteria THRU All American Engineering Co., XZS2G-1, Report N-308 |
Box 50: Aerojet Engineering, Proposal to BuAer for the Development & Manufacturing of the Aerojet Model X60AL-8000 THRU Bell Aircraft Corp., Model D-31, Navy Night Fighter Proposal, Report D31-947-001 |
Box 51: Bell Aircraft Corp., Model L-39-1, Report 33-941-701, Stress Analysis of Navy Swept Back Wing Version P-63 THRU Bell Aircraft Corp., S-114790 |
Box 52: Boeing Aircraft, Model 400-2-2, Preliminary Information, Scout Aircraft for the U.S. Navy BAR, D-6628 THRU Boeing Aircraft, Model 441 Single Engine Trainer, Report WD12032 |
Box 53: Boeing Aircraft, Model 441 Single Engine Trainer, Report WD12033, Specifications for Preparing Drawing & Data Lists THRU Boeing Aircraft, Model 442-1, Class VSN, Report WD-12047, Issue #2, Preliminary Study, Boeing Wichita |
Box 54: Boeing Aircraft, Model 442-1, Class VSN, Report WD-12047, Issue #3, Preliminary Study, Boeing Wichita THRU Columbia Aircraft, XJL-1 |
Box 55: Consolidated Vultee Aircraft, Class VB, Carrier Based Bomber THRU Consolidated Vultee Aircraft, VF (N) Proposal, Navy Night Fighter, Report DEVF 1442 Stability& Control Characteristics Twin Westinghouse 24C Engine |
Box 56: Consolidated Vultee Aircraft, VF (N) Proposal, Navy Night Fighter, Report DEVF 2016 Weight & Balance Data THRU Consolidated Vultee Aircraft, Navy Tailless Design, 2 P & W R4600 Engines, Report ZW-014 |
Box 57: Consolidated Vultee Aircraft, Class VB, Navy Search Landplane THRU Consolidated Vultee Aircraft, Class VP Patrol Seaplane 4 R2800 Engines, Report ZW-017, Preliminary Weight & Balance Estimate |
Box 58: Consolidated Vultee Aircraft, Navy Patrol Seaplane 4 R2800 Engines, Photos [Model], K-293 to K-302 THRU Consolidated Vultee Aircraft, XPB3Y-1, Class VPB, Patrol Bomber, ZW-34-002, Appendix to Report ZW-34-001 |
Box 59: Consolidated Vultee Aircraft, Class VP, Model 34, 4 Engine Long Range Flying Boat, Report ZD-34-001 THRU Consolidated (Vultee) Aircraft, Model XP5Y-1 Airplane, Class VP Long Range Patrol Seaplane, Report 8347 |
Box 60: Consolidated Vultee Aircraft, Report ZP-44-15005, Class VP Patrol Seaplane 4 R-2800-14 Engines THRU Curtiss-Wright Airplane Div, Columbus, ASW Proposal #20, Design Proposal [2 of 6] |
Box 61: Curtiss-Wright Airplane Div, Columbus, ASW Proposal #20, Design Proposal [3 of 6] THRU Curtiss-Wright, VFN Proposal, Report, Vol. I, General Design [2 of 2] |
Box 62: Curtiss-Wright, VFN Proposal, Report, Vol. II, Detailed Specifications, Ditching Characteristics [1 of 2] THRU Curtiss-Wright, General Design Data, VF-1, Vol. 2, Detail Specifications Add. To SR-36 & 38, April 1946 [Duplicate] |
Box 63: Curtiss-Wright, General Design Data, VF-1, Vol. 3, Weight & Balance Estimate VF, Report 21206, April 1946 THRU Curtiss-Wright, VF-2 General Design Data, Vol. 3, April 1946, Weight & Balance Estimate VF-2 |
Box 64: Curtiss-Wright, VF-2 General Design Data, Vol. 4, April 1946, Performance Analysis of VF-2 Proposal, Report 21220 THRU Curtiss-Wright, [Class] VSB |
Box 65: Curtiss-Wright, Class VBT, Report 20192, Revised Design Proposal, June 16, 1942 THRU Curtiss-Wright, XBTC-1, Class VBT, Report 20206 |
Box 66: Curtiss-Wright, XBTC-2, Class VBT, Summary of Aerodynamic Data THRU Curtiss-Wright, Griffin Controlled Missile, Report 9546, Calculated Performance & Stability Calculations of the ""Griffin"" Proposal |
Box 67: Curtiss-Wright, Aerodynamic Design Study of the ""Lark"" Project, Report 9527 THRU Douglas Aircraft, Model 561, Report ES 6905, Performance Report, Includes Navy Calculations & Performance Charts |
Box 68: Douglas Aircraft, Model 561, Report ES 6908, Estimated Weight & Balance THRU Douglas Aircraft, DS-565, Detailed Specifications for Model 565 Airplane (Copy 4) |
Box 69: Douglas Aircraft, DS-565, Report ES 20528, Estimate of Duct Losses and their Effect Power Plant Performance THRU Douglas Aircraft, DS-566, Report ES 20549, Performance Summary |
Box 70: Douglas Aircraft, DS-566, Report ES 20551, Velocity-Altitude Characteristics & VN Diagram THRU TB2D Oct 1942 [Correspondence] |
Box 71: TB2D [Correspondence] THRU Edo Aircraft, Edo Report #1802, Proposed Weight & Balance, Class XVSN |
Box 72: Edo Aircraft, Edo Report #1803, Longitudinal Stability Characteristics, Class XVSN (1 of 2) THRU Edo Aircraft, Proposal, Class VSN, Single Engine Seaplane, Model XOSE-1, Report 1706, Revised Performance |
Box 73: Edo Aircraft, Proposal, Class VSN, Single Engine Seaplane, Model XOSE-1Report 1706/1800, Estimated Performance THRU Edo Aircraft, Model XS2E-1, Report 1702, Estimated Performance Normal Scout Bomber wt 5200 lb |
Box 74: Edo Aircraft, Model XS2E-1 Airplane, Instrument Panel Mockup Photos (4) THRU Fairchild Aircraft, Model M-92, Report 92014, Detailed Specifications Primary-Basic Trainer [1 of 2] |
Box 75: Fairchild Aircraft, Model M-92, Report 92014, Detailed Specifications Primary-Basic Trainer [2 of 2] THRU Globe, VSO, R-1820, Comment D.C. |
Box 76: Goodyear Aircraft, Proposal GA-13, Report GER-88, Estimated Weight & Balance THRU Goodyear Aircraft, Engineering Report, GA-13A, Night Fighter Airplane [1 of 2] |
Box 77: Goodyear Aircraft, Engineering Report, GA-13A, Night Fighter Airplane [2 of 2] THRU Goodyear VF R-2800 & West 24C |
Box 78: Grumman Aircraft Engineering Corp., Design 70, Single Engine Torpedo Bomber Basic THRU XF6F-1,2,3,4 [Grumman Correspondence] |
Box 79: Grumman Aircraft Engineering Corp., Design 56, A-190, Performance Calculation THRU Hughes Aircraft, Model 19, Patrol Bomber Airplane, Four Engine, Long Range, Flying Boat, No. 19-1 |
Box 80: Hughes Aircraft, Class VPB, Model 19, Patrol Bomber Flying Boat, [Report 19-103-W] Preliminary Weight & Balance THRU Lockheed Scout Observation Airplane, Evaluation of Jet Lift Hull Type VSO with V1710 H-19 Engine |
Box 81: Lockheed Scout Observation Airplane, VSO Airplane Design Study THRU Lockheed Scout Observation Airplane, VSO Airplane Design Study |
Box 82: Glenn L. Martin Co., Model 190, Air Corps Model B-33 Bomb Airplane 4 Engines, Resume of Detailed Specifications THRU Glenn L. Martin Co., Flying Boat Navy Patrol Airplane, Models 225-1 & 225-2, Report 2068, Design Comparison |
Box 83: Glenn L. Martin Co., Model 230-6 Aerodynamic Studies for Martin Navy Patrol Seaplane, Engineering Report No. 2318 THRU Glenn L. Martin Co., Comparison Table Models 364M, 212-1, 212-2 [Oversize] |
Box 84: Glenn L. Martin Co., Class VP Patrol Bomber, Model XP4M-1, Martin Meteor Landplane, No. 329, Detail Specification THRU McDonnell Aircraft, Model 24, Twin Engine Fighter with 2 Westinghouse 24C Engines, Report S-123 |
Box 85: McDonnell Aircraft, Model 24, Twin Engine Fighter, Report 258, Preliminary Performance Calculations THRU McDonnell Aircraft, Aerodynamics Report for Model 40 ,Airplane, Report #422, Plans, Drawing S-1 |
Box 86: McDonnell Aircraft, Model 40, Report 411 Aerodynamic Report for Model 40 Airplane THRU McDonnell Aircraft, Confidential Report 235, The Gargoyle |
Box 87: North American Aviation, Class VF Fighter, Report NA8375, Design Specifications for a Carrier Fighter Airplane [2 of 3] THRU North American Aviation, NA 46-333, Contractor Design. RD1386B |
Box 88: North American Aviation, NA 46-301, Contractor Design, RD1386B, Detail Specification THRU North American Aviation, T2J-1, Report NA-56H-183, Preliminary Study Advanced Trainer System, ESO CL-4035 |
Box 89: XFR-1 [Correspondence] THRU Temco Aircraft, Model 51 [TT-1], Engineering Report 52.2.74 |
Box 90: Temco Aircraft, Model TT-1, Engineering Report 51.2.75 THRU Vega Aircraft Corp., V-146, XP2V-1, R-626, Preliminary Specifications Patrol Airplane |
Box 91: Vega Aircraft Corp., V-146, XP2V-1, Land Based Patrol Bomber, R-942, Aerodynamic Comparisons THRU Vega Aircraft Corp., V-146, XP2V-1 Airplane Analysis, Design Transition |
Box 92: Vega Aircraft Corp., Model V-141 Torpedo Scout Bomber, Preliminary Design Study, Part I THRU Vought-Sikorsky Aircraft, Model VS-315, Correspondence |
Box 93: Chance Vought Aircraft, Report 6625, V-340 Detail Specification, Informal Proposal THRU Chance Vought Aircraft, VF (N) Class Proposal, V-343A, Report 5691, Duct Loss Calculations |
Box 94: Chance Vought Aircraft, VF (N) Class Proposal, V-343B, Report 5682, Performance Calculations THRU ZAP Cargo, Capt. L.C. Stevens, 1/19/44, Correspondence |
Box 95: Bendix Helicopters, [Proposal, Model SWG-1A] Navy Liaison & Reconnaissance Helicopter THRU PV Engineering Forum, PVS-12, Helicopter, Report 12-W-01 Detail Weight & Balance Statement, Class HR, Twin Rotor |
Box 96: PV Engineering Forum, PVS-14, Helicopter, Detail Specifications, Class HR, Twin Rotor (1 of 2) THRU Unidentified Drawing 89-517 ""Perspective Galley to Flight Deck,"" 1/6/1943 |
Box 97: P/A Target Proposals THRU Change Vought Aircraft, Report 6883, Determination of Loads and Stress Analysis of Target Winged Aero X-27A |
Box 98: Heavy Attack Proposals THRU VP Land Based Minelayer |
Box 99: VP Seaplane Comp, 15 April 1946 THRU VP Seaplane Comp, 15 April 1946 |