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... F-1 rocket engine F-1 and J-2 rocket engine J-2 rocket engines. The contracts provided: (1) $1 million for long lead-time items in F-1 rocket engine F-1 engine R&D; (2) $3.4 million for early production effort on 55 F-1 rocket engine F-1 engines; and (3) $1.7 million for early production work on 59 J-2 rocket engine J-2 engines ... two days of specific testimony on the Centaur program. NAA announced that the 1961 Robert J. Collier Trophy, U.S. aviation's highest honor, was awarded to four test pilots of ...

... onboard equipment was functioning normally. ''(Tass, 12/2/65)'' President Johnson named Dr. Finn J. Larsen, Honeywell vice president, as Principal Director of Defense Research and Engineering for , succeeding Dr. E. G. Fubini ... Marshall Space Flight Center MSFC to USAF Arnold Engineering Development Center, Tullahoma, Tenn., for use in high-altitude tests of the stage's J-2 engine. ''( Marshall Space Flight Center MSFC Release 65-291 ...

... &A, 9/64, 97)'' In satellite communications demonstration at AIAA Washington meetings, Lt. Cdr. J. F. Debold, Commanding Officer, U.S. Naval Research and Development Satellite Communications Group, ... Army-developed communications terminals on East and West Coasts. ''( AIAA Booster, 7/2/64, 2)'' Engineers proposed development of intercontinental ballistic troop trans-port capable of carrying 1,200 ...

... \Delta = \ q + q_1^i + q_2^j + q_3^k '''(II.1)''' where \ i, j, k are hypercomplex numbers that satisfy i^2 = j^2 = k^2 = −ijk = −1, \ −ij = ji = k, \ −jk = kj = i, \ −ki = ik = j '''(II.2)''' The quantity \ q ...

... >File:Ordway Disc 20 Pt 1.mp4 Ordway Tape Series Number: Series J-2, J-3 Wernher von Braun, Willy Prasthofer, Rudolf Hermann, Otto Cerny, Ernst Klauss '''Interviewers on this ...

... >File:Ordway Disc 19 Pt 1.mp4 Ordway Tape Series Number: Series J-2, Wernher von Braun, Willy Prasthofer, Rudolf Hermann, Otto Cerny, Ernst Klauss '''Interviewers on this series ...

Image:R-2rocket.jpg R-2 rocket schematic Image:R-2engineering.jpg R-2 engineering facilities Image:R-2launchfacility.jpg R-2 launch facilities Image:R-2launch.jpg R-2 launch Category:Launch Vehicle

... could, on a very low density tile, expose the surface to 2,300 degrees Fahrenheit, and the backface, three inches deep, would ... our briefing on the main engines, we got it from either the Managing Engineer or the Lead Engineer or the Design Engineer. It hadn’t ... believe that, coming from America, I had never watched Dallas with J. R. Ewing. But, you know, I was busy. Laughs '''Ross-Nazzal ...

... lakebed had been flooded. '''Bobko:''' Yes, so we landed on Runway 2-2 at Edwards. You know, it’s a big runway. There wasn’ ... , after my flight, I was in my office and P. J., P. J. Paul J. Weitz, who was my first commander, called me up and said, ... . What was the interaction like between the astronaut corps and the engineers and other parts of NASA? '''Bobko:''' I think usually very favorable. ...

... Branch. It was a mishmash of about ten engineers. Milt Milton L. Windler was one of them, I remember. There was Walt Walter J. Kapryan, who later became the launch director at ... they were basically running into a wind-shear problem as they got up to the 2,000-foot altitude where the descent started. Wind shears, at certain days, would actually put ... together a little bit, which made me wonder how you as an engineer in operations worked with the engineers from Engineering and Development Directorate , those guys under Max Faget who, you said at ...

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