Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor-Reference-Cited by-同舟云学术

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Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor

Published:2017-11 Issue: Volume:140 Page:247-254
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Tian Hui,Yu Ruipeng,Zhu Hao,Wu Junfeng,Cai Guobiao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Hybrid rocket development history;Altman,1991

2. Hybrid rocket engines: the benefits and prospects;Davydenko;Aerosp. Sci. Technol.,2013

3. Hybrid rocket development at the American Rocket Company;Kniffen,1990

4. Design and development of a 100 km nitrous oxide/paraffin hybrid rocket vehicle;Dyer,2007

5. Optimal design of hybrid rocket motor powered vehicle for suborbital flight;Cai;Aerosp. Sci. Technol.,2013

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1. Chemical Species involved in Hypergolic Ignition of a Green Hybrid Rocket Propellant;AIAA SCITECH 2024 Forum;2024-01-04

2. Numerical and experimental research on axial injection end-burning hybrid rocket motors with polyethylene fuel;Chinese Journal of Aeronautics;2023-12

3. Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine;Journal of Propulsion and Power;2023-09

4. Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence;Journal of Propulsion and Power;2023-07

5. Ignition processes and characteristics of charring conductive polymers with a cavity geometry in precombustion chamber for applications in micro/nano satellite hybrid rocket motors;Defence Technology;2023-05

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