Nuclear safety considerations for manned space flight
Nuclear safety considerations for ground checkout, launch and in-orbit operations of reactors for earth orbital manned space stations
Gerrels, E. E.↗
Engineering topics
Stafford, W. H.
Publications and source records attributed to Stafford, W. H..
Preliminary analysis of a wake trailing a spacecraft
Using void regions trailing orbiting bodies to conserve propellant of untethered modules flying in formation with mother spacecraft
Butcher, J. R.↗
Performance analysis of chemical stages in the 300 to 400 second specific impulse range for interplanetary missions
Effect of thrust-weight ratios and specific impulses on trajectory parameters for earth orbit hyperbolic escape and entry
TRAJECTORY ANALYSIS↗
Performance analysis of chemical stages in the 300 to 400 second specific impulse range for interplanetary missions
Trajectory parameters for escaping from & braking into earth orbit utilizing single vehicle stage with high specific impulse
SPECIFIC IMPULSE↗
Orbital parameters for artificial earth satellites up to 40,000 km altitude
Graphs for circular and transfer orbits up to 40,000-km. altitude
ORBIT CALCULATION↗
Motion of the sub-satellite point for 24-hour orbits
Subsatellite path for 24-hour orbits affected by changes in eccentricity, inclination, and argument of perigee - orbital path of syncom ii
SYNCOM II SATELLITE↗
PERFORMANCE ANALYSIS OF HIGH-ENERGY CHEMICAL STAGES FOR INTERPLANETARY MISSIONS. PART III- BRAKE TO MARS ORBIT
Chemical propulsion for interplanetary flight and design of spacecraft for braking into orbit around planet mars
MARS /PLANET/↗