Boost-phase equilibrium pressures in a dual- thrust solid-propellant rocket motor
Author:
Affiliation:
1. Emerson Electric Co., St. Louis, Mo.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28241
Reference5 articles.
1. Solid Propellant Rockets
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1. Experimental Investigation of Dual-Thrust Rocket Motor with Intermediate Nozzle;Journal of Propulsion and Power;2017-09
2. Experimental and theoretical study on a dual-thrust rocket motor with subsonic intermediate nozzle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-04-30
3. Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle;Journal of Propulsion and Power;2017-03
4. Investigation of Dual-Thrust Rocket Motor with Subsonic Intermediate Nozzle;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23
5. Burn-back Equations for High Volumetric Loading Single-grain Dual-thrust Rocket Propellant Configuration;Defence Science Journal;2011-02-11
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