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Utilization of Residual Helium to Extend Satellite Lifetimes and Mitigate Space Debris
- Source :
- Journal of Propulsion and Power. 28:1406-1412
- Publication Year :
- 2012
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2012.
-
Abstract
- A new electric propulsion device concept takes advantage of residual helium gas that is trapped in the chemical propellant feed system and currently unused at end of life. The helium ion thruster provides additional propellant resources to extend satellite lifetimes and transfer geostationary orbit space assets to ultrasafe disposal orbits. The predicted capability, if fully allotted to the disposal, allows for perigee heights above the geostationary altitude that are one order of magnitude greater than existing international guidelines of 250 km. Furthermore, the proposed helium ion thruster concept makes the classic propellant gauge uncertainty problem moot, as satellite operators could use all of their conventional propellant for nominal station-keeping operations. The helium ion thruster concept therefore mitigates future space debris arising from depleted assets in the geostationary orbit belt through both aggressive orbit raising and depressurization of satellites at end of life. An analysis of the helium ion thruster theoretical performance shows that the device could raise the altitude of an end-of-life 2500 kg, 5 kW spacecraft by 2200 km in two months using 2 kg of residual helium.
- Subjects :
- Physics
Propellant
Ion thruster
business.industry
Mechanical Engineering
Aerospace Engineering
High Power Electric Propulsion
Fuel Technology
Propellant mass fraction
Electrically powered spacecraft propulsion
Space and Planetary Science
Physics::Space Physics
Geostationary orbit
Satellite
Aerospace engineering
business
Space debris
Subjects
Details
- ISSN :
- 15333876 and 07484658
- Volume :
- 28
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi...........5c28e295937cd58de6a2014a7ed65f69