Add to ORKGThe three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Details of the program, the vehicles, the payloads, the firings, the tracking, and the results are presented. Principal result was the first experimental verification of a confined radiation zone of the type postulated by Van Allen and others
Spacecraft performance, control, and flight path analysis of Lunar Orbiter 3 extended missio
The nuclear electric propulsion (NEP) concept design developed in support of the Space Transfer Conc...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
The Little Joe II Qualification Test Vehicle, Model 12-50-1, was launched from Army Launch Area 3 {A...
Communications and television subsystems and radar equipment for Mars 1969, 1971, and 1975 and Venus...
The capability of an Ultra Distributed Energy Store System (UDESS) powered electromagnetic launcher ...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
Design, fabrication, installation, and operation of X ray diffractometer and X ray spectrograph syst...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
An angular-scanning large-aperture (36 cm) backscatter lidar was developed and deployed on the NASA ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
Digital computer program for IBM 7094 computer to generate spacecraft tracking station calculation
The HIPES Program was conducted for NASA-LeRC by TRW. The Basic Program consisted of system studies,...
General and specific quantitative and qualitative results were identified from a study of actual ope...
Spacecraft performance, control, and flight path analysis of Lunar Orbiter 3 extended missio
The nuclear electric propulsion (NEP) concept design developed in support of the Space Transfer Conc...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
The Little Joe II Qualification Test Vehicle, Model 12-50-1, was launched from Army Launch Area 3 {A...
Communications and television subsystems and radar equipment for Mars 1969, 1971, and 1975 and Venus...
The capability of an Ultra Distributed Energy Store System (UDESS) powered electromagnetic launcher ...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
Design, fabrication, installation, and operation of X ray diffractometer and X ray spectrograph syst...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
An angular-scanning large-aperture (36 cm) backscatter lidar was developed and deployed on the NASA ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
Digital computer program for IBM 7094 computer to generate spacecraft tracking station calculation
The HIPES Program was conducted for NASA-LeRC by TRW. The Basic Program consisted of system studies,...
General and specific quantitative and qualitative results were identified from a study of actual ope...
Spacecraft performance, control, and flight path analysis of Lunar Orbiter 3 extended missio
The nuclear electric propulsion (NEP) concept design developed in support of the Space Transfer Conc...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio