Experimental Investigation of Dual-Thrust Rocket Motor with Intermediate Nozzle-Reference-Cited by-同舟云学术

Experimental Investigation of Dual-Thrust Rocket Motor with Intermediate Nozzle

Published:2017-09 Issue:5 Volume:33 Page:1285-1293
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

El-Nady A. M.¹,Ahmed M. Y. M.¹,El-Senbawy M. A.¹,Sarhan A. M.²

Affiliation:

1. Military Technical College, Cairo 11311, Egypt

2. Modern Academy at Maadi, Cairo 11838, Egypt

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36233

Reference7 articles.

1. SmolikF. L., Theory and Design of Rockets, Military Technical College Press, Cairo, 1967, pp. 148–164.

2. Boost-phase equilibrium pressures in a dual- thrust solid-propellant rocket motor

3. “Dual-Chamber Controllable Solid Propellant Rocket Motor, Volume 1—Research and Development Efforts,” Air Force Rocket Propulsion Lab. Rept. TR-65-209, California, Nov. 1965.

4. Dual-chamber rocket motor operating characteristics

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