Possible storable propellant configurations and program plans are evaluated for the space tug. Alternatives examined include: use of existing expendable stages modified for use with shuttle, followed by a space tug at a later date; use of a modified growth version of existing expendable stages for greater performance and potential reuse, followed by a space tug at a later date; use of a low development cost, reusable, interim space tug available at shuttle initial operational capability (IOC) that could be evolved to greater system capabilities at a later date; and use a direct developed tug with maximum potential to be available at some specified time after space shuttle IOC. The capability options were narrowed down to three final options...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
A research and development program was successfully completed towards the development of a method of...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
The cost and programmatic considerations which integrate mission requirements and architectural opti...
The mechanical extension of the human operator to remote and specialized environments poses a series...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
The Jupiter Orbiter as it is presently understood is documented. Because the Jupiter Orbiter Probe 1...
An energetic experiment using the Z80 family of microcomputer components is described. Data collecte...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
A preliminary feasibility study of the microwave multi-applications payload (MMAP) system for the Sp...
A nitrogen supply subsystem based on the dissociation of hydrazine into a mixture of hydrogen and ni...
The Mars Rover Laser Scanning system uses a precision laser pointing mechanism, a photodetector arra...
Tracking and data acquisition system (TDAS) requirements, TDAS architectural goals, enhanced TDAS su...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
Numerical analysis of acceleration flight data of Mariner Mars 69, OAO 2, and ATS to determine distu...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
A research and development program was successfully completed towards the development of a method of...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
The cost and programmatic considerations which integrate mission requirements and architectural opti...
The mechanical extension of the human operator to remote and specialized environments poses a series...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
The Jupiter Orbiter as it is presently understood is documented. Because the Jupiter Orbiter Probe 1...
An energetic experiment using the Z80 family of microcomputer components is described. Data collecte...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
A preliminary feasibility study of the microwave multi-applications payload (MMAP) system for the Sp...
A nitrogen supply subsystem based on the dissociation of hydrazine into a mixture of hydrogen and ni...
The Mars Rover Laser Scanning system uses a precision laser pointing mechanism, a photodetector arra...
Tracking and data acquisition system (TDAS) requirements, TDAS architectural goals, enhanced TDAS su...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
Numerical analysis of acceleration flight data of Mariner Mars 69, OAO 2, and ATS to determine distu...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
A research and development program was successfully completed towards the development of a method of...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...