Add to ORKGThe conceptual design of the Jupiter probe spectrometer is presented. Block and circuit diagrams are presented along with tabulated parts lists. Problem areas are considered to be (1) the schedule, (2) weight limitations for the electronic systems, and (3) radiation hardness of the electronic devices
The design and performance of pointing and control systems for two space infrared telescope facility...
Tests carried out in November 1981 on the stationary flap of STOL test planes at Kakuda Labs are des...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
Conceptual design studies were performed directed toward a high power, ultralightweight solar array,...
The feasibility and conceptual design aspects of repair materials and procedures for in orbit repair...
Doppler and ranging data routinely generated at the Deep Space Stations of the California Institute ...
Voyager project - mission analysis, evaluation of spacecraft systems, reliability, and exploration o...
A portable microcomputer data system was developed to test a 2 x 64-element Si:Bi charge injection d...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Within the simulation limitations of on-orbit conditions, it was demonstrated that a helium purge sy...
The charactertistics and performance capability of the current Viking '75 Gas Chromatograph/Mass Spe...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
The design and performance of pointing and control systems for two space infrared telescope facility...
Tests carried out in November 1981 on the stationary flap of STOL test planes at Kakuda Labs are des...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
Conceptual design studies were performed directed toward a high power, ultralightweight solar array,...
The feasibility and conceptual design aspects of repair materials and procedures for in orbit repair...
Doppler and ranging data routinely generated at the Deep Space Stations of the California Institute ...
Voyager project - mission analysis, evaluation of spacecraft systems, reliability, and exploration o...
A portable microcomputer data system was developed to test a 2 x 64-element Si:Bi charge injection d...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Within the simulation limitations of on-orbit conditions, it was demonstrated that a helium purge sy...
The charactertistics and performance capability of the current Viking '75 Gas Chromatograph/Mass Spe...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
The design and performance of pointing and control systems for two space infrared telescope facility...
Tests carried out in November 1981 on the stationary flap of STOL test planes at Kakuda Labs are des...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...