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Lots 3292, 3815, 3815, 3875, 3954, 4032, 4033, 4157, 4163, 4166, 4168, 4247, 4249, 4250, 4316, 4577, 4604, 4608, 4610, 4618, 4660, 4846-4850, 4913, 4922-4926, 5109-5112, 5211-5217, 5432, 5396-5398, 5411, 5412, 5415, 5416, 5432-5434, 5472-5475, 5477, 5478, 5481, 5483, 5511, 5512, 6126-6130. Manned Spacecraft Center prepared a Statement of Work to be accomplished by Air Force Space Systems Division (SSD) in its role as contractor to NASA for the procurement of Titan II launch vehicles for the Gemini program. Manned Spacecraft Center completed an analysis of possible power sources for the Gemini spacecraft.
NASA-MSC, Gemini Project Note of January 23, 1962, Subj: Summary of Analysis for Selecting the Power Source for the Gemini Project, Jan. Manned Spacecraft Center notified Marshall Space Flight Center, Huntsville, Alabama (which was responsible for managing NASA's Agena Programs) that Project Gemini required 11 Atlas-Agenas as rendezvous targets and requested Marshall to procure them. Air Force Space Systems Division issued a Technical Operating Plan to Aerospace Corporation, El Segundo, California, for support of the Gemini Launch Vehicle Program; a contract followed on March 15. Aerospace, Draft of Annual Report, Fiscal 1962-63, undated; Harris, Gemini Launch Vehicle Chronology, pp. Memo, Tindall to Walter C Williams, Subj: Consolidation of Gemini Computer Programming and Operation at Houston, Texas, Feb 19, 1962. AiResearch Manufacturing Company, a division of the Garrett Corporation, Los Angeles, California, received a $15 million subcontract from McDonnell to manufacture the environmental control system (ECS) for the Gemini spacecraft. The initial coordination meeting between Gemini Project Office and McDonnell was held at Manned Spacecraft Center, Houston.
McDonnell Report 8635, Gemini Spacecraft-Crew Station System Specification, Feb 20, 1962, rev. Martin-Baltimore submitted its initial proposal for the redundant flight control and hydraulic subsystems for the Gemini launch vehicle; on March 1, Martin was authorized to proceed with study and design work. Conclusion of Meeting of NASA, SSD, Martin, McDonnell, Mar 2, 1962; Harris, Gemini Launch Vehicle Chronology, pp. McDonnell let a $32 million subcontract to North American Aviation's Rocktdyne Division, Sacramento, California, to build liquid propulsion systems for the Gemini spacecraft. Representatives of McDonnell, North American, Manned Spacecraft Center, and NASA Headquarters met to begin coordinating the interface between spacecraft and paraglider.
Manned Spacecraft Center (MSC) suballotted $5.2 million to Marshall Space Flight Center for procuring Atlas-Agena vehicles for Project Gemini. Memo, Johnson for All Concerned, Subj: Preliminary Description of Simulators and Training Equipment Expected to be used in Project Gemini, Mar. Westinghouse Electric Corporation, Baltimore, Maryland, received a $6.8 million subcontract from McDonnell to provide the rendezvous radar and transponder system for the Gemini spacecraft. McDonnell awarded a $6.5 million subcontract to Minneapolis-Honeywell Regulator Company, Minneapolis, Minnesota, to provide the attitude control and maneuvering electronics system for the Gemini spacecraft. Gemini Project Office accepted McDonnell's preliminary design of the spacecraft's main undercarriage for use in land landings and authorized McDonnell to proceed with detail design. Manned Spacecraft Center directed North American to design and develop an emergency parachute recovery system for both the half-scale and full-scale flight test vehicles required by Phase II-A of the Paraglider Development Program and authorized North American to subcontract the emergency recovery system to Northrop Corporation's Radioplane Division, Van Nuys, California. Marshall Space Flight Center delivered an Agena procurement schedule (dated March 8) to Gemini Project Office.
Gemini Project Office (GPO) decided that seat ejection was to be initiated manually, with the proviso that the design must allow for the addition of automatic initiation if this should later become a requirement. Gemini Project Office restated its intention to use Project Mercury hardware and subcontractors for Gemini. McDonnell awarded AiResearch a $5.5 million subcontract to provide the reactant supply system for the Gemini spacecraft fuel cells. Advanced Technology Laboratories, Inc, Mountain View, California, received a $3.2 million subcontract from McDonnell to provide the horizon sensor system for the Gemini spacecraft. Thiokol Chemical Corporation, Elkton, Maryland, received a $400,000 sub-contract from McDonnell to provide the retrograde rockets for the Gemini spacecraft. Air Force Space Systems Division awarded a letter contract to Aerojet-General Corporation, Azusa, California, for the research, development, and procurement of 15 propulsion systems for the Gemini launch vehicle, as well as the design and development of the related aerospace ground equipment.
McDonnell awarded a $4.475 million subcontract to the Western Military Division of Motorola, Inc, Scottsdale, Airzona, to design and build the digital command system (DCS) for the Gemini spacecraft. Air Force Space Systems Division published the "Development Plan for the Gemini Launch Vehicle System".
McDonnell awarded a $2.5 million subcontract to Collins Radio Company, Cedar Rapids, Iowa, to provide the voice communications systems for the Gemini spacecraft.
Martin-Baltimore submitted a "Description of the Launch Vehicle for the Gemini Spacecraft" to Air Force Space Systems Division. Martin Report ER-12209, "Description of the Launch Vehicle for the Gemini Spacecraft," Rev.
Representatives of Manned Spacecraft Center, Ames Research Center, Martin, and McDonnell met to discuss the participation of Ames in the Gemini wind tunnel program.
ACF Electronics Division, Riverdale, California, of ACF Industries, Inc., received a $1 million subcontract from McDonnell to provide C- and S-band radar beacons for the Gemini spacecraft. Earl Whitlock of McDonnell presented a "Gemini Manufacturing Plan" (dated April 6) to Gemini Project Office (GPO). Manned Spacecraft Center confirmed that a five-day orbital lifetime of Agena systems would be adequate for currently planned missions. Martin-Baltimore and Air Force Space Systems Division (SSD) reported to Gemini Project Office on the problems of establishing abort criteria for the malfunction detection system (MDS). NASA announced that applications would be accepted for additional astronauts until June 1, 1962. McDonnell awarded a $26.6 million subcontract to International Business Machines (IBM) Corporation's Space Guidance Center, Owego, New York, to provide the computer system for the Gemini spacecraft. Studebaker Corporation's CTL Division, Cincinnati, Ohio, received a subcontract for $457,875 from McDonnell to provide two backup heatshields for the Gemini spacecraft, similar in material and fabrication technique to those used in Project Mercury. At an Atlas-Agena coordination meeting, Lockheed presented a comprehensive description of its proposed propulsion development plans for the Gemini-Agena. Representatives of North American, NASA Headquarters, Langley Research Center, Flight Research Center, Ames Research Center, and Manned Spacecraft Center met to review the design and testing philosophy for the half-scale test vehicle (HSTV) in phase II-A of the Paraglider Development Program. Minutes of Meeting of Paraglider Development Program (Phase II-A) Half Scale Test Vehicle Design Review, May 16, 1962; NAA Report SID65-196, "Final Report of Paraglider Research and Development Program, Contract NAS 9-1484," Feb.
McDonnell proposed to evaluate the Gemini redezvous radar and spacecraft maneuvering system on early flights by using a rendezvous evaluation pod to be ejected from the spacecraft in orbit. MSC, Weekly Activity Report for the Office of the Director, Manned Space Flight, June 24-30, 1962, p.
Air Force Space Systems Division (SSD) awarded a letter contract to Lockheed Missiles and Space Company for eight Agena vehicles to be modified as Gemini Agena target vehicles (GATV).
Lockheed LMSC - A605200-2 and -7, Gemini Agena Target Vehicle Program Progress Reports: October 1964, p. Following a Lockheed briefing on pulse-code-modulation (PCM) instrumentation systems, representatives of Goddard Space Flight Center and Manned Spacecraft Center (MSC) formed a small working group to discuss the feasibility of making the Gemini telemetry system a full PCM system.
Gemini Project Office directed McDonnell to determine what would be involved in opening and closing the spacecraft hatches in the space environment and Manned Spacecraft Center's Life Systems Division to determine what special pressure suit features would be required to provide crew members with a 15-minute extravehicular capability.
Manned Spacecraft Center's Life Systems Division proposed to measure seven parameters for determining crew condition during all Gemini flights. The postlanding survival kit proposed for use by Gemini crew members would be basically similar to the one used in Project Mercury.

Representatives of McDonnell, Northrop Ventura (formerly Radioplane), Weber Aircraft, and Manned Spacecraft Center attended the first ejection seat design review at McDonnell in St Louis. At a mechanical systems coordination meeting, representatives of McDonnell and Gemini Project Office decided to develop more powerful retrograde rocket motors for the Gemini spacecraft. McDonnell subcontracted the parachute landing system for Gemini to Northrop Ventura at an estimated cost of $1,829,272. McDonnell awarded an $8 million subcontract to Electro-Mechanical Research, Inc., Sarasota, Florida, to provide the data transmission system for the Gemini spacecraft. Representatives of McDonnell and Manned Spacecraft Center completed a series of 24 meetings to negotiate the technical details of McDonnell's plans for supporting and documenting Project Gemini, specifications for Gemini systems and subsystems, environmental and structural design criteria for the spacecraft, spacecraft performance specifications, test programs, and plans for reliability, quality assurance, and validation. Ames Research Center began the first wind tunnel test of the half-scale inflatable paraglider wing in support of the Paraglider Development Program.
Manned Spacecraft Center concurred in McDonnell's proposed sequencing of the paraglider recovery system. Abstracts of Meetings on Mechanical Systems, May 19 and 25, 1962; Abstract of Meeting on Spacecraft-Paraglider Interface, Mar.
North American began a test program to qualify the emergency parachute system for the half-scale flight test vehicle required for Phase II-A of the Paraglider Development Program. Representatives of McDonnell, Weber Aircraft, Gemini Procurement Office, Life Systems Division, Gemini Project Office, and US Naval Ordnance Test Station, China Lake, California, concluded plans for development testing of the spacecraft ejection seat. A list of the aerospace ground equipment required to handle and check out the Gemini spacecraft before flight was presented at the first spacecraft operations coordination meeting. The Air Force School of Aviation Medicine, Brooks Air Force Base, Texas, began a simulated long-duration Gemini mission. NASA-Defense Purchase Request T-8630-G, June 25, 1962; Life Systems Division Weekly Activity Report, June 8, 1962. McDonnell was authorized to procure an additional boilerplate spacecraft for parachute landing system tests.
Whirlpool Corporation Research Laboratories, St Joseph, Michigan, received a contract from Manned Spacecraft Center (MSC) to provide the Project Gemini food and waste management system, comprising water dispenser, food storage, and waste storage components.
Manned Spacecraft Center authorized North American to go ahead with Phase II, Part B(1), of the Paraglider Development Program. A paraglider full-scale test vehicle Design Engineering Inspection was held at North American's Space and Information Systems Division in Downey, California. Gemini Project Office reported that a thorough study of the reentry tracking histories of the Mercury-Atlas 4, 5, 6 and 7 missions had been completed. After considering Gemini related investigations that might be carried out with the help of Mercury, Gemini Project Office and McDonnell decided that the most useful would be testing heatshield materials and afterbody-shingle characteristics.
McDonnell and North American representatives met for the first time to exchange detailed technical information on the installation of the paraglider in the spacecraft. Martin-Baltimore's airborne systems functional test stand went into operation at Baltimore. Gemini Project Office met with representatives of Manned Spacecraft Center's Flight Operations Divisions, McDonnell, International Business Machines, Aerospace, Air Force Space Systems Division, Lockheed, Martin, Space Technology Laboratories, Inc. Memo, James F Dalby to Acting Chief, FOD, Subj: Coordination of Effort of Contractors Performing Guidance and Trajectory Studies for Project Gemini, July 3, 1962. Martin prepared a plan for flight testing the malfunction detection system (MDS) for the Gemini launch vehicle on development flights of the Titan II weapon system. The capability for successfully accomplishing water landings with either the parachute landing system or the paraglider landing system was established as a firm requirement for the Gemini spacecraft.
Representatives of Gemini Project Office (GPO), Flight Operations Division, Air Force Space System Division, Marshall Space Flight Center, and Lockheed attended an Atlas-Agena coordination meeting in Houston.
At technical team at Air Force Missile Test Center, Cape Canaveral, Florida - responsible for detailed launch planning, consistency of arrangements with objectives, and coordination - met for the first time with official status and a new name.
To ensure mechanical and electrical compatibility between the Gemini spacecraft and the Gemini-Agena target vehicle, Gemini Project Office established an interface working group composed of representatives from Lockheed, McDonnell, Air Force Space Systems Division, Marshall, and Manned Spacecraft Center.
Gemini Project Office and North American agreed on guidelines for the design of the advanced paraglider trainer, the paraglider system to be used with static test article No. NASA Administrator James E Webb announced officially that a new mission control center for manned space flight would be established at Manned Spacecraft Center (MSC) in Houston. McDonnell reported reducing the rated thrust of the two forward-firing thrusters from 100 pounds to 85 pounds to reduce disturbance torques generated in the event of maneuvers with one engine out.
A reliability review of the Titan II launch vehicle engine system was held in Sacramento, California, at Aerojet-General's Liquid Rocket Plant, the site where the engines were being developed. Lockheed presented study findings and design recommendations on the Agena D propulsion systems to representatives of Marshall, Manned Spacecraft Center, and Air Force Space Systems Division in a meeting at Houston. North American began a test program to qualify the emergency parachute recovery system for the full-scale test vehicle in Phase II-A of the Paraglider Development Program. At a meeting in Los Angeles, the Air Force described to Gemini Project Office its plans for converting complex 14 at Atlantic Missile Range, Cape Canaveral, Florida. Flight Control Operations Branch of Manned Spacecraft Center's Flight Operations Division outlined a program of training for Gemini flight controllers.
North American began flight tests of the half-scale vehicle (HSTV) in Phase II-A of the Paraglider Development Program two months behind schedule. Manned Spacecraft Center (MSC) formally reviewed McDonnell's engineering mock-up of the Gemini spacecraft in St Louis. The Air Force and NASA agreed to use a standard Atlas space booster for the Gemini program, sharing the development cost equally. Gemini Project Office initiated a program to coordinate and integrate work on developing Gemini rendezvous and long-duration missions. At a spacecraft production evaluation meeting, Gemini Project Office and McDonnell revised the projected launch date of the first Gemini flight from August to September 1963. Rocketdyne completed designing and fabricating prototype hardware for both spacecraft liquid propulsion systems and initiated testing of the reaction control system. A Medaillen zum Gedenken Martin Luthers und der Reformation - Luther - Ehrung auf MA?nzen und Medaillen. A Die Medaillen-und MA?nzsammlung der Lutherhalle - Reformations-MA?nzen und Medaillen, Ausstellung in der Staatlichen Lutherhalle Wittenberg 1983.
A Sonderausstellung der Reformations-Medaillensammlung Adolf Bruns und andere GegenstA¤nde. A Auktion 371: MA?nzen der Antike, Islam, Ausland, Brandenburg-Preussen, Sachsen, Hanau, Hessen aus Slg. A Auktion 32: Griechische und RA¶mische MA?nzen, MA?nzen und Medaillen der Niederlande, Numismatische Literatur.
The launch vehicle would retain the general aerodynamic shape, basic systems, and propulsion concepts of the missile.
Potential problem areas in pulse-code-modulated (PCM) telemetry, the bipropellant attitude and control system, and time required to install electrical components and wiring had not yet affected the launch schedule.
The operating principle of the fuel cell designed by General Electric, adopted for use in the Gemini spacecraft. Tindall, Jr., Flight Operations Division, requested consolidation of all Gemini computer programming and operation at Manned Spacecraft Center in Houston. Block diagram of the Gemini environmental control system, subcontracted by McDonnell to AiResearch Manufacturing Co.

Johnson, Head of the Spacecraft Operations Branch of Manned Spacecraft Center's Flight Crew Operations Division, circulated a memorandum on proposed training devices for Project Gemini.
The location of the main elements of the rendezvous radar system on the Gemini spacecraft and the Agena target vehicle. A functional block diagram of the attitude control and maneuvering electronics system of the Gemini spacecraft. Gemini spacecraft communications system, which received ground commands for transfer to spacecraft systems. Illustrating the stages of a mission during which various elements of the Gemini spacecraft communications system would be used. Petersburg, Florida, Aeronautical Division of Minneapolis-Honeywell received an $18 million subcontract from McDonnell to provide the inertial measuring unit (IMU) for the Gemini spacecraft.
Goodrich Company, Akron, Ohio, a cost-plus-fixed-fee contract for $209,701 to design, develop, and fabricate prototype pressure suits.
The parachute recovery system to be used instead of paraglider on the first Gemini spacecraft: stowed and deployed modes. 6 to the Gemini launch vehicle procurement contract assigned $2.609 million to fund the construction necessary to convert pad 19 at Cape Canaveral for Gemini flights.
The emergency parachute recovery system for the half-scale paraglider flight test vehicle for Phase II-A of the development program. Two McDonnell technicians examine the engineering mockup of the Gemini spacecraft, exhibited to 140 industry and NASA representatives in St. Schmid.A  Die MA?nzen der freien Reichsstadt Augsburg von erlangtem MA?nzrecht (1521) an bis zum Verluste der Reichsfreiheit (1805).
Nagy of NASA Headquarters because the twin stars Castor and Pollux in constellation Gemini (the Twins) seemed to him to symbolize the program's two-man crew, its rendezvous mission, and its relation to Mercury. It was distributed at the same time NASA announced that the project was to be named "Gemini." (NASA Photo S-62-88, released Jan. Scheduled launch dates were adjusted, however, because program approval had come a month later than originally anticipated in the Project Development Plan. Although any system selected would require much design, development, and testing effort, the fuel cell designed by General Electric Company, West Lynn, Massachusetts, appeared to offer decided advantages in simplicity, weight, and compatiblity with Gemini requirements over solar cells or other fuel cells. The Gemini flight trainer (above) would simulate the entire mission, while the docking trainer (below) would simulate the final stages of rendezvous. The seats were to be used before launch (off-the-pad abort) or during the first phase of powered flight (to about 60,000 feet) if the launch vehicle malfunctioned.
15; McDonnell, "Project Gemini Monthly Progress Letter Report, 26 June 1962 thru 25 July 1962," undated, p. 16-17; Rocketdyne mimeo, "Gemini Propulsion by Rocketdyne - A Chronology," May 15, 1967, p. Martin LUTHER en andere voortreflyke mannen, zedert den jare 1515 en vervolgens, in Duitschland en de aangrenzende ryken door Godts zegen gewrocht. A ISBN 978-3-7774-4235-8 A Reformation-related medals on pages 13-15, 22, 23, 36, 37, 90-95, 14, -147, 191-193, 196-211. Coincidentally, the astronomical symbol (II) for Gemini, the third constellation of the zodiac, corresponded neatly to the Mark II designation. The Statement of Work accompanied a purchase request for $27 million, dated January 5, 1962, for 15 Titan launch vehicles.
The first flight was now planned for late July or early August 1963 with six-week launch centers between the first three flights. A basic feature of the General Electric design, and the source of its advantages over its competitors, was the use of ion-exchange membranes rather than gas-diffusion electrodes. Goodrich, "Design, Development, and Fabrication of Prototype Pressure Suits Final Report," Feb.
PCM Instrumentation Coordination Meeting, May 7, 1962; NASA Eighth Semiannual Report to Congress, July 1-December 31, 1962, pp. 8, 1962; Supplemental Proposal, Contracts NAS 9-167 and NAS 9-539, Paraglider Phase II A and Phase II B(1), June 11, 1963, p. Lots 1319, 1343-1353, 1674, 1678, 1896, 1906-1910, 1926-1928, 1930, 1982, 2065, 2147-2153, 6627.
Pending ratification of the Gemini Operational and Management Plan, however, funding was limited to $3 million. Subsequent launches would occur at two-month intervals, with the last flight in late April or early May 1965. On March 20, 1962, McDonnell let a $9 million subcontract to General Electric to design and develop fuel cells for the Gemini spacecraft. 31; Lockheed Report LMSC 447186-26, Medium Space Vehicles Programs Monthly Progress Report, August 1962, Sept.
A Lots 541, 542, 569, 570, 675, 687, 780, 781, 788, 808, 832, 916, 917, 1016, 1065, 1178, 1227. To oversee this work, SSD established a Gemini Launch Vehicle Directorate, headed by Colonel Richard C. It was responsible for planning and directing all technical activities and all contractor activities within the scope of the contract. LotsA 1269, 1367, 1399-1401, 1466, 1476, 1482, 1483, 1498-1502, 1514, 1562-1564, 1609, 1643, 1718, 1719, 1876, 2051, 2100, 2124, 2179, 2181, 2223, 2455, 2456, 2525. Lots 4733, 4823, 4827, 4847, 4861, 4884, 4891, 4901-4908, 4922-4926, 4954, 4962, 4968, 5081, 5106, 5135, 5153, 5159, 5175, 5294, 5295, 5600-5603, 5739. Lots 7002, 7009, 7010, 7016, 7017, 7018, 7019, 7020, 7021, 7029, 7030, 7034, 7035, 7046, 7047, 7050. Lots 4042a, 4160, 4192, 4202, 4204, 4255, 4296, 4332, 4407-4409, 4457, 4505, 4617, 4700, 4702, 4705, 4706, 5215a, 5408e. 9-10 (hereafter cited as Lockheed Agena Monthly Report); Lockheed, LMSC-A766871, Gemini Agena Target Press Handbook, Feb.
Lots 2139, 2954, 2955, 2966, 2981, 3453-3455, 3465, 3780, 3818, 4015, 4016, 4044, 4046, 4047, 4102, 4103, 4140-4144, 4154-4156, 4378. A Lots A 683, 1047, 1139, 1213, 1243, 1325-1340, 1385-1387, 1396-1398, 1527, 1528, 1541, 1556, 1559, 1594, 1603-1605, 1640, 1791-1796, 1861-1863, 2056, 2057, 2096-2100. A Lots A 668, 669, 1495, 1957, 1960, 2007, 2045, 2067, 2084, 2174, 2181, 2184-2189, 2245, 2302, 2315, 2326, 2327, 2357, 2358, 2367, 2381, 2382, 2475, 2600, 2685-2689, 2970, 2971, 2982, 2983. Initial budgeting and planning were completed by the end of March, and a final Statement of Work was issued May 14; although amended, it remained in effect throughout the program. Lots 3180, 3207, 3383, 3532, 3574, 3580-3585, 3599, 3603, 3737, 3903, 3904, 3992, 4029, 4030, 4283-4286, 4338, 4358, 4719, 4855.
Lots 2959-2964, 2988, 2999-3001, 3108-3112, 3148, 3177, 3221, 3446, 3590, 3626, 3810, 3811, 3918, 4338. 1 were components of the instrument and recording system and the inertial platform; for spacecraft No.
Goodrich to produce four successively improved prototypes of an advanced full-pressure suit, and two prototypes of a partial-wear, quick-assembly, full-pressure suit.

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