Data return advantages of Earth-Mars-Earth trajectories.
Data return advantages of earth-Mars-earth flyby trajectories over more conventional Mars trajectories
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Data return advantages of earth-Mars-earth flyby trajectories over more conventional Mars trajectories
Close flyby trajectory calculations around planets with return to earth capability
Translunar abort technique for nonfree-return missions
Entry aerodynamics at lunar return conditions from command module of Apollo 4 flight
Pyrotechnic activated calorimeter for reentry package design of vehicles entering earth atmosphere at lunar return velocities
Deep space data return, discussing system function, design, operational interfaces and interplanetary spacecraft data compression methods
Doppler echo from random rough surface, discussing average power return, frequencies, amplitudes, antenna beamwidth and radar data correlation
Automated mars surface sample return /AMSSR/ mission, discussing Saturn 5 chemical and nuclear approach
Thermocouple vacuum gauge joined to Apollo lunar sample return containers /ALSRC/, describing two step welding procedure with transition cylinder
High resolution electron return beam vidicon cameras, comparing transfer functions and SNR with photographic films
Technique, incorporated into set of three computer programs, provides economic methodology for reducing all parameters to financially sound common denominator of present worth, and calculates resultant rate of return on new equipment, processes, or systems investments.
Measuring radar sea return as function of wave height and wind speed for fully developed seas
Alternative mission/system approaches to automated Mars surface sample return based on utilization of Titan 3 or Saturn Intermediate-20 launch vehicles
Engineering analysis of Surveyor 3 parts returned by Apollo 12 astronauts to determine lunar environment effects
Outbound and inbound stage weight requirements for planetary sample return mission payload and energy requirements - graphs
Returned Surveyor 3 camera visor examined for alpha radioactive deposit formed by decay of radon isotopes diffusing out of lunar surface
Appendices to engineering evaluation tests of Surveyor 3 television camera returned from moon by Apollo 12 astronauts - Vol. 2
Use of orbit-to-orbit shuttles for hyperbolic rendezvous with returning interplanetary spacecraft