Abstract
This chapter covers the development of cold gas microthruster, which is widely regarded as the simplest way of generating thrust in space, for nanosatellites. A brief background and principles of operation were given, followed by the introduction of nozzle theory that could be used in the preliminary estimation of microthruster performance and considerations in selecting a suitable propellant. The current state of development in cold gas microthruster (at the time of writing in 2020) was provided, from its first use in SNAP-1 in 2000 to another 12 nanosatellites as well as one technology demonstration mission in Prototype Research Instruments and Space Mission technology Advancement small satellite. The chapter ends with a discussion on future nanosatellite missions that will feature a cold gas microthruster system and the challenges, such as fabrication of micronozzle and its design optimization, to improve overall efficiency.
Original language | English |
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Title of host publication | Space Micropropulsion for Nanosatellites |
Subtitle of host publication | Progress, Challenges and Future |
Publisher | Elsevier |
Pages | 23-50 |
Number of pages | 28 |
ISBN (Electronic) | 9780128190371 |
ISBN (Print) | 9780128190388 |
DOIs | |
Publication status | Published - 2022 |
Bibliographical note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-careOtherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.
Keywords
- Cold gas
- CubeSat
- MEMS
- Micronozzle
- Microthruster