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Displaying 21—30 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
... in increasing the performance of hydrogen fueled rocket engines." P&W is producer of RL-10 liquid hydrogen rocket engines for Saturn S-IV stage and Centaur upper stage booster ...
... date 38,000 lbs. (including S-IV upper stage) and would flight-test performance of RL-10 liquid hydrogen engines of S-IV stage. ''(UPI, Wash. Post, 12/13/63)''
Rep ...
... , and the 90,000-lb.-thrust upper stage ( S-IV ) powered by six liquid-hydrogen' RL-10 engines separated and burned properly for eight minutes; attaining orbital speed. The orbited body ...
... FY 1965. The new engine would be based on results of experimental fluorine program with RL-10 engine. ''(M&R, 2/17/64, 18)''
Congressional Joint Atomic Energy Committee had sent ...
... time. The sixth, partially-achieved objective was ignition and burn of Centaur stage's two RL-10A3 liquid hydrogen engines: They ignited properly but cut off 127 sec. before programmed 380 ...
... out as much as 5,000 mi. from earth; however, the attempt to restart the RL-10 engines failed and the stage began to tumble and roll. After about 15 hr ...
... out of the Saturn I program included: "1. First extensive use of multi-engines (six RL-10 -A3's) and liquid hydrogen in the upper stages. "2. Advancement of guidance and ...
... produced 389,000 lbs, thrust at liftoff. The Centaur 2nd stage was powered by two RL-10 liquid hydrogen-liquid oxygen engines with a thrust of 15,000 lbs, each. The ...
... rights in all inventions made, or to be made, under NASA contract, which involved the RL-10 rocket engine. ‘‘(KB)’’
Two major changes effected by reorganization of activities of NASA Lewis ...
... of Headquarters program authority from NASA OMSF to Office of Space Science and Applications OSSA . RL-10 , which had powered Saturn 1's 2nd stage (S-IV) in six successful flights ...
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