Direct Underreaching Transfer Trip Testing – Technical Summary
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Vehicle requirements and mission planning for manned space flight and exploration of mars during 1975-1985 time period
State of u.s. technology for a manned exploration of mars, including bioastronautics and communications programs, tidal history of mars and financial limitations of the space program
Function and performance of instrumentation and telemeter equipment aboard Nike-Apache sounding rocket flight numbers 14.79 UE through 14.82 UE
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Weight and energy requirements of vehicle systems for manned exploration of Mars
Minimum propellant consumption trajectories to Mars for constant-thrust, constant-specific impulse vehicles with optimum coasting periods
Venus swingby used to decelerate manned spacecraft returning from Mars
Experiences in checking production of ultrahigh vacuum systems at contractor establishment
Communication parameters associated with Martian flyby probes and with lander and manned vehicles
Outer casing blowing and bleeding and undistorted inlet flow for improved performance of high aspect ratio transonic rotor
Crawler transport for moving Saturn 5 mobile rocket launcher complete with umbilical tower
Launch window variation using circular and elliptical parking orbits and transfer techniques, discussing Venus and Mars flyby missions