Add to ORKGPayload capabilities of Saturn IB-Centaur for launch opportunities to Mars in 1971, 1973, and 1975 and to Venus in 1972 and 197
A collection of optimum trajectory and spacecraft data is presented for unmanned interplanetary miss...
Mariner Jupiter-Saturn '77 mission objectives for Saturn are considered which affect the trajectory ...
The Saturn V launch vehicle represented a jump in capability for heavy lift launch vehicles, enablin...
"NASA TM X-1327.""Lewis Research Center, Cleveland, Ohio.""December 1966"--Cover.Includes bibliograp...
Selected mission concepts for interplanetary exploration through 1985 were examined, including: (1)...
The interplanetary trajectory characteristics for missions to Uranus, which employ an intermediate s...
Both the Department of Defense and NASA have clearly defined missions for the Saturn which cannot be...
A dual flyby mission to the planets and satellite systems of Jupiter and Saturn is being planned for...
Trajectory opportunities have been identified for free return manned flyby, or encounter, missions t...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
Feasible solar probes from present planned vehicle technology - saturn rocket - centaur vehicl
Mars orbiter/landing capsule mission launched by Saturn IB/SV vehicle - conceptual desig
Titan/Centaur is NASA's last new expendable launch vehicle prior to the advent of the space shuttle....
Centaur launch vehicle for Jupiter and Saturn orbiter missions using solar electric propelled spacec...
Centaur is currently the world\u27s only operational highenergy upper stage, and is the United State...
A collection of optimum trajectory and spacecraft data is presented for unmanned interplanetary miss...
Mariner Jupiter-Saturn '77 mission objectives for Saturn are considered which affect the trajectory ...
The Saturn V launch vehicle represented a jump in capability for heavy lift launch vehicles, enablin...
"NASA TM X-1327.""Lewis Research Center, Cleveland, Ohio.""December 1966"--Cover.Includes bibliograp...
Selected mission concepts for interplanetary exploration through 1985 were examined, including: (1)...
The interplanetary trajectory characteristics for missions to Uranus, which employ an intermediate s...
Both the Department of Defense and NASA have clearly defined missions for the Saturn which cannot be...
A dual flyby mission to the planets and satellite systems of Jupiter and Saturn is being planned for...
Trajectory opportunities have been identified for free return manned flyby, or encounter, missions t...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
Feasible solar probes from present planned vehicle technology - saturn rocket - centaur vehicl
Mars orbiter/landing capsule mission launched by Saturn IB/SV vehicle - conceptual desig
Titan/Centaur is NASA's last new expendable launch vehicle prior to the advent of the space shuttle....
Centaur launch vehicle for Jupiter and Saturn orbiter missions using solar electric propelled spacec...
Centaur is currently the world\u27s only operational highenergy upper stage, and is the United State...
A collection of optimum trajectory and spacecraft data is presented for unmanned interplanetary miss...
Mariner Jupiter-Saturn '77 mission objectives for Saturn are considered which affect the trajectory ...
The Saturn V launch vehicle represented a jump in capability for heavy lift launch vehicles, enablin...