Ignition delay studies on hybrid propellants
Author:
Affiliation:
1. Indian Institute of Science, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27984
Reference4 articles.
1. Ignition and thermal behaviour of solid hydrazones
2. The role of surface reactions in hypergolic ignition of liquid-solid systems
3. Ignition of Hybrid Rocket Fuels with Fuming Nitric Acid as Oxidant
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1. Effect of Fuel Activation Energy on Ignition of Hydrogen Peroxide Hybrid Rocket;Journal of Spacecraft and Rockets;2021-11
2. Spontaneously Igniting Hybrid Fuel-Oxidiser Systems.;Defence Science Journal;1995-01-01
3. NN bonded polymers;Progress in Polymer Science;1993-01
4. Effect of Variables on Ignition Delays of hydrazone/nitric acid systems;Propellants, Explosives, Pyrotechnics;1980-10
5. Studies on the Combustion of Solid Hydrazones with Nitric Acid;Propellants, Explosives, Pyrotechnics;1980-08
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