Dynamic performance of Surveyor throttleable engine when propellantscontain dissolved helium.
BRESHEARS, R. R. /CALIFORNIA INST. OF TECH., JET PROPULSION LAB., PASADENA, CALIF./,, MCCAFFERTY, J. /TRW, INC., TRW SYSTEMS GROUP, LOS ANGELES, CALIF./., MCDERMOTT, C. E. /HERCULES, INC., CHEMICAL PROPULSIONDIV., BACCHUS, UTAH/,
JOURNAL OF SPACECRAFT AND ROCKETS ; 4 , 5 ; 669-673
1967-01-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
AXISYMMETRIC, THROTTLEABLE NON-GIMBALLED ROCKET ENGINE
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