Challenges of Ablatively Cooled Hybrid Rockets for Satellites or Upper Stages
Ablative-cooled hybrid rockets could potentially combine a similar versatility of a liquid propulsion system with a much simplified architecture. These characteristics make this kind of propulsion attractive, among others, for applications such as satellites and upper stages. In this paper, the use...
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| Format: | Article |
| Language: | English |
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MDPI AG
2021-07-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/8/7/190 |