Final flight performance prediction for Saturn AS-206 /mission 276/ propulsion system S-1B-6 stage
Final flight performance prediction for Saturn AS-206, Mission 276, propulsion system, S-1B-6 stage
Koser, G. W.↗
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Final flight performance prediction for Saturn AS-207 /mission 276/ propulsion system S-1B-7 stage
Final flight performance prediction for Saturn AS-207, mission 276, propulsion system, S-1B-7 stage
Elfers, J. P.↗
Successful restart of a cryogenic upper-stage vehicle after coasting in earth orbit
Successful engine restart in space of upper stage vehicle using cryogenic propellants
Baud, K. W.↗
Effect of variable stator area on performance of a single stage turbine suitable for air cooling. 4 - Stator overall performance with 70 percent design area
Performance tests of stator component in closed position and effects on performance of single stage turbine suitable for air cooling
Behning, F. P.↗
Experimental performance of a 5-inch single-stage axial-flow turbine designed for a Brayton cycle space power system
Performance of single stage, axial flow turbine designed for Brayton cycle space power system
Futral, S. M., Jr.↗
POGO stability of the Saturn V second flight-stage.
Saturn 5 second flight stage /S-2/, investigating POGO oscillations by linear mathematical models of system
Licht, B. W.↗
A Peculiar Galaxy that May Be at a Young Evolutionary Stage
Integral sign galaxy with ionized gas and no nuclear concentration of stars, discussing evolutionary stage on basis of red shift and velocity field
Burbidge, E. M.↗
Structural research and development for cryogenic upper stages. II.
Research and development in structural and thermal analysis, materials and fabrication techniques for spacecraft upper stages utilizing cryogenic propellants
Dixon, H. H.↗
Navigation and guidance of a hypersonic/rocket two-stage launch vehicle for a rendezvous mission.
Navigation and guidance of two stage hypersonic/ rocket spacecraft launch vehicle for rendezvous mission
Retka, J. A.↗
Performance of a Mars soft lander with staged propulsion.
Performance and feasibility of staged propulsion during terminal phase of Mars soft landing
Ginsberg, L. J.↗
Propellant behavior during venting in an orbiting Saturn S-IVB stage.
Liquid hydrogen propellant dynamic and thermodynamic behavior during task venting in orbiting Saturn S-4B stage
Madsen, R. A.↗
The S II injection stage for the Mars/Venus flyby mission.
Hydrogen filled Saturn 2 injection stage assembled with flyby mission spacecraft in earth orbit for Mars/Venus flyby mission
Morita, W. H.↗
Comparison of reticular and cochlear multiple unit activity with auditory evoked responses during various stages induced by anesthetic agents. II.
Anesthesia stages induced by pentobarbital, halothane, ether or nitrous oxide, recording EEG, gross behavior, auditory evoked response and multiple unit activity
Mori, K.↗
Automation in Saturn I first stage checkout.
Hardware and software systems in automated Saturn 1 first stage checkout
Funderburk, B. J.↗
Automatic checkout systems for stages of the Saturn V manned space vehicle.
Automatic checkout systems for Saturn 5 manned space vehicle stages
Schmidt, D. M.↗
Spherical rocket motors for space and upper stage propulsion.
Spherical solid propellant rocket motor design for space and upper stage propulsion, describing empirical equations and computer program
Andrews, W. G.↗
Effect of variable stator area on performance of a single-stage turbine suitable for air cooling. 5 - Stator detailed losses with 70 percent design area
Effect of variable stator with area design of 70 percent on performance of single stage turbine suitable for air cooling
Bider, B.↗
Effect of variable stator area on performance of a single-stage turbine suitable for air cooling. 6 - Turbine performance with 70-percent design stator area
Variable stator area effect on performance of single stage turbine suitable for air cooling
Prust, H. W., Jr.↗