Nasa to launch sert i spacecraft news release no. 64-167
Spin stabilization and ion thrustor engines for space electric rocket test /sert/ spacecraft
SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Spin stabilization and ion thrustor engines for space electric rocket test /sert/ spacecraft
Space electric rocket tests /sert/ which will provide data for systems design, including neutralization of space ion beams and qualification of electric thrustors for mission applications
Space electric rocket test /sert/ and early electric propulsion systems
Description and operation of spacecraft in space electric rocket test /sert/ thrustor flight test
Evaluation of Thorad-Agena systems during ascent to orbit and Agena orbital performance during SERT 2 mission
Space electric rocket test /SERT/ II thrustor system, discussing flight worthiness and mercury bombardment discharges
Space electric rocket test /SERT/ II thrustor system, discussing flight worthiness and mercury bombardment discharges
Mercury bombardment ion thrustor life test in space environment onboard space electric rocket test /SERT/ satellite, describing passive satellite thermal control system design
Ion thrustor flight test using SERT I spacecraft flown into trajectory by Scout Launch vehicle
Stress analysis for reliability of NASA-Lewis electron bombardment thrustor used in Sert 1 spacecraft
Spacecraft systems design, dynamics, ground support equipment, testing, and reliability for SERT program for ion beam neutralization in ion propulsion engine
Thrust detection systems on space electric rocket test ion thrustors
Power conditioning system for ion engine used in Sert-I flight test
Optimum discharge chamber configuration of permanent magnet mercury-bombardment thrustor for SERT II mission
Mercury fed plasma bridge neutralizers for in- flight operation of SERT II electron bombardment ion thrustor