NIMBUS SPACECRAFT SYSTEM CONCEPT
Nimbus satellite - systems design - data acquisition - television transmission - orbital mechanics
ORBITAL MECHANICS↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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NIMBUS SPACECRAFT SYSTEM DEVELOPMENT
Nimbus satellite - systems analysis - sensory ring contents - management planning
MANAGEMENT↗
PROTECTION REQUIREMENTS FOR THE RESISTANCE OF METEORITE PENETRATION OF INTERPLANETARY SPACECRAFT SYSTEMS
Meteoroid flux - nature and distribution of & micrometeoroid model for meteoroid hazard study
METEOROID HAZARD↗
LUNAR EXPLORATION AND SPACECRAFT SYSTEMS
Proceedings of the american astronautical societys lunar-flight symposium held on december 27, 1960
SPACE SCIENCE↗
The nimbus spacecraft system
Nimbus satellite timing, sensory, ground control, and data transmission systems
GROUND CONTROL↗
The nimbus spacecraft system
Explore the source record for details and available documents.
Press, H.↗
Voyager spacecraft system Task C summary Final technical report, Apr. 1966 - Jul. 1967
Mission planning, orbit determination, thrust vector control, and configuration management program for Voyager project - summary
VOYAGER PROJECT↗
Voyager spacecraft system Task C mission risk analysis study. Volume I - Summary Volume II - Development. Volume III - Handbook Final technical report, Apr. 1966 - Jul. 1967
Iterative risk analysis approach for assessing and comparing risks associated with proposed Voyager missions
VOYAGER PROJECT↗
Voyager spacecraft system Task C configuration data and management study Final technical report, Apr. 1966 - Jul. 1967
Configuration identification data and management procedures for Voyager project
VOYAGER PROJECT↗
Voyager spacecraft system Task C thrust vector control study Final technical report, Apr. 1966 - Jul. 1967
Liquid insertion thrust vector control system for Voyager project
VOYAGER PROJECT↗
Apollo spacecraft systems analysis program. Range coverage for the CSM rendezous radar transponder. Antenna raised 4 in. and tilted forward 15 deg
Range coverage diagrams for CSM rendezvous radar transponder antenna raised 4 in. and tilted forward 15 deg
Doty, M. G.↗
Apollo spacecraft systems analysis program. A comparison of the computed LR received signal spectrum and the 1967 PEARL data
Similarities between experimentally measured power spectral density curves of landing radar signal returned from rough surface and computer simulated curves for sinusoidal surfaces
Chambers, D. E.↗
Apollo spacecraft systems analysis program. Landing radar altimeter beam bandwidth and Doppler equations for mathematical model use
Lunar reflectivity, acquisition altitude, landing radar altimeter beam bandwidth, and Doppler equations verified for use in mathematical model
Blakely, C. E.↗
Apollo Spacecraft Systems Analysis Program. Analysis of Rendezvous Radar Pearl Flight Test Data
Flight test data analysis for rendezvous radar performance during simulated lunar mission
Dobby, S. D.↗
Apollo spacecraft systems analysis program. Preliminary LR reflectivity model
Preliminary lunar reflectivity graphs
Dickerson, E. T.↗
Surveyor Spacecraft System - Surveyor 7 Flight Performance Final Report
Performance analyses of Surveyor 7 lunar probe including launch, orbit, descent, photography, alpha scattering measurements, and soil sampling
Source record↗
Apollo Spacecraft Systems Analysis Program. Task E-34E - LM Landing Radar Performance over Rough Terrain
Performance prediction for LM landing radar over rough terrain
Sappington, J. N.↗