The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would demonstrate the use of electric ion thrusters for long-term (5 yr) station keeping and attitude control of a synchronous orbit satellite. Other mission objectives included in the study were: station walking to satellite rendezvous and inspection, use of low cost attitude sensing system, use of an advanced solar array orientation and slip ring system, and an ion thruster integrated directly with a solar array power source. The SERT D spacecraft, if launched, will become SERT 3 the third space electric thruster test
Interest in the application of primary solar-electric propulsion to high-energy Earth orbital and de...
Design constraints, design description, handling and fabricating, and shock and vibration testing of...
NASA is developing mission concepts for a solar electric propulsion technology demonstration mission...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
The results of testing the flight thrusters on the SERT spacecraft during the 1974 test period are p...
Design criteria for integrating electric propulsion system into SERT 2 spacecraft and future spacecr...
The flight results obtained from mid 1979 through December 1980 are presented. Near continuous solar...
The historical record of the SERT II ion thrusters and spacecraft performance for 6 1/2 years since ...
The University of Alabama in Huntsville's (UAH) Propulsion Research Center hosted the Space Solar Po...
The conference provided a forum to assess critical needs and technologies for the NASA electrochemi...
Procedures for determining launch window for SERT 2 mission and effect of low thrust and earth oblat...
Description and operation of spacecraft in space electric rocket test /sert/ thrustor flight tes
The SERT 2 satellite, launched in February, 1970, has recently been reactivated after being dormant ...
This paper describes mainly the 1997 version of the Solar EUV Rocket Telescope and Spectrograph (SER...
This document contains the proceedings of NASA's fourth Space Electrochemical Research and Technolog...
Interest in the application of primary solar-electric propulsion to high-energy Earth orbital and de...
Design constraints, design description, handling and fabricating, and shock and vibration testing of...
NASA is developing mission concepts for a solar electric propulsion technology demonstration mission...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
The results of testing the flight thrusters on the SERT spacecraft during the 1974 test period are p...
Design criteria for integrating electric propulsion system into SERT 2 spacecraft and future spacecr...
The flight results obtained from mid 1979 through December 1980 are presented. Near continuous solar...
The historical record of the SERT II ion thrusters and spacecraft performance for 6 1/2 years since ...
The University of Alabama in Huntsville's (UAH) Propulsion Research Center hosted the Space Solar Po...
The conference provided a forum to assess critical needs and technologies for the NASA electrochemi...
Procedures for determining launch window for SERT 2 mission and effect of low thrust and earth oblat...
Description and operation of spacecraft in space electric rocket test /sert/ thrustor flight tes
The SERT 2 satellite, launched in February, 1970, has recently been reactivated after being dormant ...
This paper describes mainly the 1997 version of the Solar EUV Rocket Telescope and Spectrograph (SER...
This document contains the proceedings of NASA's fourth Space Electrochemical Research and Technolog...
Interest in the application of primary solar-electric propulsion to high-energy Earth orbital and de...
Design constraints, design description, handling and fabricating, and shock and vibration testing of...
NASA is developing mission concepts for a solar electric propulsion technology demonstration mission...