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Extinction–reignition superiority in a single-stage sounding hybrid rocket

  • Published:2016-11 Issue: Volume:58 Page:437-444
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Chiba Kazuhisa,Yoda Hideyuki,Kanazaki Masahiro,Shimada Toru

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Advanced hybrid rockets for future space launch;Karabeyoglu,2013

2. High performance hybrid propulsion system for small satellites;Simurda,2013

3. Handling considerations of nitrous oxide in hybrid rocket motor testing;Thicksten,2008

4. Suborbital and low-thermospheric experiments using sounding rockets in Taiwan;Chern;Acta Astronaut.,2012

5. Combustion of liquefying hybrid propellants: Part 1, general theory;Karabeyoglu;J. Propuls. Power,2002

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