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Effect of Fuel-to-Oxidiser Ratio on Thrust Generation of a Hybrid Al + NaOH + H2O Propulsion System for CubeSat Applications
File(s)
Author(s)
Ahmed, O
Knoll, AK
Type
Conference Paper
Date Issued
2016-05-02
Date Acceptance
2016-03-01
Citation
Proceedings of Space Propulsion Conference 2016
URI
Journal / Book Title
Proceedings of Space Propulsion Conference 2016
Copyright Statement
© the authors
Source
Space Propulsion Conference 2016
Start Date
2016-05-02
Coverage Spatial
Rome, Italy