Add to ORKGDirect and indirect Atlas Centaur booster ascent mode comparisons for Mars flyby spacecraf
Centaur is currently the world\u27s only operational highenergy upper stage, and is the United State...
Launch window characteristics of Jupiter opportunities using Atlas Centaur launch vehicl
Titan/Centaur is NASA's last new expendable launch vehicle prior to the advent of the space shuttle....
"NASA TM X-1181"--Cover."Lewis Research Center, Cleveland, Ohio"--Cover."November 1965"--Cover.Inclu...
Lunar launch data - ascent characteristics of Atlas-Centaur AC-15 configuration and mission ground r...
Parametric data, systems analyses, and space capsule design concepts - direct versus orbital entry f...
Parametric design of interplanetary and orbital trajectories with examples for Mars 1973, 1975, and ...
Titan 3 launch vehicle performance and flight mechanics analyses - direct versus orbital entry for M...
Payload capabilities of Saturn IB-Centaur for launch opportunities to Mars in 1971, 1973, and 1975 a...
Round trip missions to Mars have been investigated to define representative launch windows and assoc...
Generalized equations and in-flight computer requirements for Centaur guidance and control and advan...
Machine computations of three-dimensional ballistic interplanetary trajectories - June, July, and Au...
Entry and terminal phase performance analyses of configurations for direct versus orbital entry for ...
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
Comparison of Atlas-Centaur /Surveyor/ and iterative guidance mode guidance concept
Centaur is currently the world\u27s only operational highenergy upper stage, and is the United State...
Launch window characteristics of Jupiter opportunities using Atlas Centaur launch vehicl
Titan/Centaur is NASA's last new expendable launch vehicle prior to the advent of the space shuttle....
"NASA TM X-1181"--Cover."Lewis Research Center, Cleveland, Ohio"--Cover."November 1965"--Cover.Inclu...
Lunar launch data - ascent characteristics of Atlas-Centaur AC-15 configuration and mission ground r...
Parametric data, systems analyses, and space capsule design concepts - direct versus orbital entry f...
Parametric design of interplanetary and orbital trajectories with examples for Mars 1973, 1975, and ...
Titan 3 launch vehicle performance and flight mechanics analyses - direct versus orbital entry for M...
Payload capabilities of Saturn IB-Centaur for launch opportunities to Mars in 1971, 1973, and 1975 a...
Round trip missions to Mars have been investigated to define representative launch windows and assoc...
Generalized equations and in-flight computer requirements for Centaur guidance and control and advan...
Machine computations of three-dimensional ballistic interplanetary trajectories - June, July, and Au...
Entry and terminal phase performance analyses of configurations for direct versus orbital entry for ...
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
Comparison of Atlas-Centaur /Surveyor/ and iterative guidance mode guidance concept
Centaur is currently the world\u27s only operational highenergy upper stage, and is the United State...
Launch window characteristics of Jupiter opportunities using Atlas Centaur launch vehicl
Titan/Centaur is NASA's last new expendable launch vehicle prior to the advent of the space shuttle....