Session
Technical Session VIII: University Student Scholarship Competition
Abstract
Using reconfigurable and adaptable networks of micro/nanosatellites to support cost-effective space missions is a popular new direction in the space community. Since the overall resources of micro/nanosatellites are more restricted than those of a single large satellite, the micropropulsion system needs to be lightweight, low-cost, and practical. This paper describes the collaboration between the Arizona State University Student Satellite Lab and the Air Force Research Laboratory Propulsion Directorate to flight test a micropropulsion system on a nanosatellite, ASUSat2. The motivation behind this conjuncture is to employ university satellites as an inexpensive testbed for unconventional new technologies. This paper first provides background on the needs of a micropropulsion system on a micro/nanosatellite cluster, and outlines the issues concerning its development. Then it addresses the experience of the ASU group in designing and building nanosatellites, and describes the design and mission of ASUSat2, which is part of a three-satellite constellation. Next, it examines two micropropulsion systems, the free molecule micro-resistojet and the cold-gas micronozzle, for the ASUSat2 mission. The preliminary study shows that the free molecule micro-resistojet would be an attractive micropropulsion system for ASUSat2.
The University Micro/Nanosatellite as a Micropropulsion Testbed
Using reconfigurable and adaptable networks of micro/nanosatellites to support cost-effective space missions is a popular new direction in the space community. Since the overall resources of micro/nanosatellites are more restricted than those of a single large satellite, the micropropulsion system needs to be lightweight, low-cost, and practical. This paper describes the collaboration between the Arizona State University Student Satellite Lab and the Air Force Research Laboratory Propulsion Directorate to flight test a micropropulsion system on a nanosatellite, ASUSat2. The motivation behind this conjuncture is to employ university satellites as an inexpensive testbed for unconventional new technologies. This paper first provides background on the needs of a micropropulsion system on a micro/nanosatellite cluster, and outlines the issues concerning its development. Then it addresses the experience of the ASU group in designing and building nanosatellites, and describes the design and mission of ASUSat2, which is part of a three-satellite constellation. Next, it examines two micropropulsion systems, the free molecule micro-resistojet and the cold-gas micronozzle, for the ASUSat2 mission. The preliminary study shows that the free molecule micro-resistojet would be an attractive micropropulsion system for ASUSat2.
