Radiation effects on composite structures Final report
Radiation and temperature effects on composite structures in Pegasus satellite
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Radiation and temperature effects on composite structures in Pegasus satellite
Military and NASA programs are discussed in which FCC were used. Included are Saturn 4, Pegasus satellites solar, array for Skylab orbital workshop, Poseidon missiles, MK 48 torpedo fire control, and Lunar Surveyor.
Plans to attach removable panels to Pegasus C satellite to study space environment
Rare earth metals and compounds as material of thermoelectronic cathodes postflight trajectory for Saturn I /SA-8/ Pegasus B test flight
Postflight trajectory analysis and orbital flight discussion for Saturn I /SA- 9/ launch vehicle carrying Pegasus payload
NASA press kit - launch preparations for Pegasus C, meteoroid detector panels
Orbital mission of Pegasus B payload with Apollo boilerplate spacecraft, launched by Saturn SA-8 - summary
Elastomeric methyl silicone polymer thermal control coating evaluation with Pegasus spacecraft
Power system developments for rockets and space flights - fuel cells, improved zinc-silver oxide battery, brushless dc motors, switching transformer regulator, and Pegasus electricity
Electronic and micrometeoroid detector panels for Pegasus thermal design
Space environment degradation of thermal control coatings tested by experimental packages on Pegasus I, II and III
Data collection and analysis of meteoroid penetration recorded on Pegasus flights, and derived flux figures
Pegasus measurements of temperature, radiation, and rigid body motion
Test tool to simulate critical portions of Pegasus meteoroid detector electronics
Pegasus thermal control louver system characteristics determined by environmental chamber testing, noting testing configuration
Thermal control coating degradation data from aluminum case containing four sensors aboard Pegasus spacecraft
Pegasus meteorite-detecting satellite design and performance and data on meteorites
Use of attitude information for Pegasus-type meteoroid puncture counting satellite to infer probable radiant and puncture flux enhancement