Most space missions require on-board propulsion systems and these systems are often dominant spacecraft mass drivers. Presently, on-board systems account for more than half the injected mass for commercial communications systems and even greater mass fractions for ambitious planetary missions. Anticipated trends toward the use of both smaller spacecraft and launch vehicles will likely increase pressure on the performance of on-board propulsion systems. The acceptance of arcjet thrusters for operational use on commercial communications satellites ushered in a new era in on-board propulsion and exponential growth of electric propulsion across a broad spectrum of missions is anticipated. NASA recognizes the benefits of advanced propulsion and NASA's Office of Space Access and Technology supports an aggressive On-Board Propulsion program, including a strong electric propulsion element, to assure the availability of high performance propulsion systems to meet the goals of the ambitious missions envisioned in the next two decades. The program scope ranges from fundamental research for future generation systems through specific insertion efforts aimed at near term technology transfer. The On-Board propulsion program is committed to carrying technologies to levels required for customer acceptance and emphasizes direct interactions with the user community and the development of commercial sources. This paper provides a discussion of anticipated missions, propulsion functions, and electric propulsion impacts followed by an overview of the electric propulsion element of the NASA On-Board Propulsion program.
[1]
Roger M. Myers,et al.
Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping
,
1997
.
[2]
J. Polk,et al.
A 5,730-hr cyclic endurance test of the SPT-100
,
1995
.
[3]
N. Maslennikov,et al.
SPT-100 subsystem development status and plan
,
1994
.
[4]
Paul Lichon,et al.
Development and demonstration of a 600-second mission-average I(sp) arcjet
,
1996
.
[5]
Roger M. Myers,et al.
Advanced propulsion for geostationary orbit insertion and north-south station keeping
,
1995
.
[6]
Pavlos Mikellides,et al.
Modeling of ablation-fed pulsed plasma thrusters
,
1995
.
[7]
John R. Brophy,et al.
Endurance Testing and Fabrication of Advanced 15-cm and 30-cm Carbon-Carbon Composite Grids
,
1995
.
[8]
Roger M. Myers,et al.
Pulsed Plasma Thruster Technology for Small Satellite Missions
,
1995
.
[9]
David C. Byers,et al.
New Developments and Research Findings: NASA Hydrazine Arcjets
,
1994
.