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Displaying 1—10 of 42 matches for query "RL-l0" retrieved in 0.000 sec with these stats:
- "rl" found 55 times in 38 documents
- "l0" found 5 times in 5 documents
... stages, exclusive of inertial guidance system being developed by Honeywell Co., and liquid hydrogen-fueled RL-l0 engine being built by Pratt & Whitney Div. of United Aircraft Corp. ''(NASA Release 64 127 ...
... . NASA Michoud Operations, where Saturn stages are fabricated.
Liquid hydrogen-liquid oxygen engine RL-10 rocket engine RL-10 A3 completed its preliminary flight rating test, Marshall Space Flight Center MSFC announced. RL-10A3 was advanced version of RL-10 rocket engine RL-10 A1, first U.S. engine using liquid hydrogen. Six A3 ...
... Pratt and Whitney Div. of United Aircraft Corp. for continuation of RL-10 rocket engine development. Contract would complete the RL-10 qualification program; it would specify improvements to be incor ... as well as certain support services to be provided to Centaur and Saturn vehicle systems. RL-10 engines were being used to propel the Centaur upper-stage launch vehicle and the ...
... rating test of the Nation's first liquid-hydrogen rocket engine. The engine, the RL-10 rocket engine RL-10 , was designed and developed by Pratt and Whitney, of United Aircraft, for ... completed within 5 days under simulated space conditions, consistently producing 15,000 pounds of thrust. RL-10, previously known as XLR-115, was initiated in October 1958 and over 700 firings ...
... conducted thrust chamber tests of high-energy upper stage rocket engine using liquid hydrogen ( RL-10 rocket engine RL-10 ).
Previous experience led NASA Lewis Research Center to design and construct experimental ...
... )''
NASA Marshall Space Flight Center awarded preliminary, 90-day
contract for development of variable-thrust RL-10 rocket engine
to Pratt and Whitney Aircraft. The hydrogen-powered engine
rated thrust and be capable of restarting in space. Throttleable
RL-10 engines had been test-fired in feasibility studies at Pratt
and Whitney plant and ...
... system underwent successful test. At General Dynamics /Astronautics Sycamore Canon test site in Calif., - two RL-10 engines underwent full duration, full power test ''(380 sec, at 30,000 lbs. thrust ... development of the Multi-Mission Module (MMM) at this time, The module would use two RL-10 engines with tanks configured for different missions. Serving as the third stage of the ...
... space vehicle, and developing and operating a checkout System.
First successful captive firing of RL-10 rocket engine RL-10 Centaur engines on a single- tank propulsion test vehicle, at Edwards Rocket ...
... supply liquid hydrogen for use on the West Coast, particularly for development of RL-10 rocket engine RL-10 engine and for the 1.2-million-pound-thrust M-1 rocket engine ...
... firing of series, which was run in vacuum chamber to simulate space environment, RL-10 rocket engine RL-10 ran nine seconds and generated a rated 15,000 pounds of thrust.
First ...
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