Performance evaluation of the hypergolic green propellants based on the HTP for a future next generation spacecrafts
Author:
Affiliation:
1. Institute of Aviation
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4849
Reference34 articles.
1. Apogee manoeuvre with a restartable liquid bipropellant motor
2. An Experimental Investigation of Hypergolic Ignition Delay of Hydrogen Peroxide with Fuel Mixtures
3. Ignition Behavior of Novel Hypergolic Materials
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