Investigations of a combustible inertial launch design
Date published
2015-06-30
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Authors
Supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
British Interplanetary Society
Department
Type
Article
ISSN
0007-084X
Format
Citation
Yemets V, Prince SA, Wilkinson R. (2015) Investigations of a combustible inertial launch design. Journal of the British Interplanetary Society, Volume 68, Issue 7, pp. 188-199
Abstract
The paper develops a subject of a combustible inertial (self-feeding) launch vehicle for nano and pico satellites. A part of the paper considers a flight of the rocket using ballistic, aerodynamic and thermal calculations. Another part describes experimental investigations of a laboratory-scale model of the rocket engine. Plans for future work and prospects of the self-feeding technology combined with pulse engine mode for microlaunchers and small satellite micro propulsion concludes the paper.
Description
Software Description
Software Language
Github
Keywords
Combustible inertial LV, Self-feeding rocket propulsion
DOI
Rights
Attribution-NonCommercial 4.0 International