Orbital elements following premature translunar injection shutdowns. Project Apollo
Orbital elements following premature translunar injection shutdowns
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Orbital elements following premature translunar injection shutdowns
Vacuum chamber heat transmission analysis
Low onset-rate energy absorber for Apollo command module couch struts
Procedures for use in transforming velocity vectors from selenographic system to mean nearest Besselian year
Effects of instrument unit platform pitch drift rates on TLI for lunar landing mission
Lunar orbit navigation and landing accuracy
Evaluating land landing problem from prelaunch measured wind effects on launch escape vehicle aborts from Saturn 1B launch vehicle
FM degradation by multipath in closed chamber
Piloted simulation of docking with various configurations of jet failures and solar panels extended or retracted
Matched conic model and integrated circumlunar trajectories compared at injection, pericynthion and perigee
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectories
Performance capability and vehicle dynamics of Saturn 5 launch vehicle for two engine out malfunctions for Saturn S-1C stage
Effect of cabin pressure on environmental control system
Onboard midcourse correction targeting during transearth phase of lunar mission
Thermal radiation effects of lunar environment on pressure-suited man on lunar surface
Data and examples for estimating deorbit parameters for out-of-plane burns and bank angle modulation
Correlating residual patterns in earth orbit unified S-band data with errors in station location or time tagging for postflight analysis
CSM-active rendezvous simulation studies using sextant and ranging device