A high performance liquid rocket engine for satellite main propulsion-Reference-Cited by-同舟云学术

A high performance liquid rocket engine for satellite main propulsion

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Stechman Carl¹,Woll Peter¹,Fuller Raymond¹,Colette Anthony¹

Affiliation:

1. Primex Aerospace Co., Redmond, WA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3161

Reference4 articles.

1. Design criteria for film cooling for small liquid-propellant rocket engines.

2. Stechman, R. Carl, "Advanced Thrust Chamber Materials for Earth Storable Bipropellant Rocket Engines".ActaAstronautica, Vol 29,No. 2pp. 109-115, 1993

3. IT. Handing, R.H. Tuffias, and R.B. Kaplan, Iridium-Coated Rhenium Thrusters by CVD". NASA TM-101309,1988.

4. R.H.Tuffias, G.J.Melden, A.J.Fortini, and J.T. Harding, "CVD Indium Process Control and Improvement and ChamberFabrication".Final Report (UL17TR-93-7154), Contract NAS3-25792, NASA LewisResearch

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