Optimization of dual-expander rocket engines in single-stage-to-orbit vehicles-Reference-Cited by-同舟云学术

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Optimization of dual-expander rocket engines in single-stage-to-orbit vehicles

Published:1997-01 Issue:2-8 Volume:40 Page:151-163
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Manski Detlef,Hagemann Gerald,Saβnick Hagen D.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. The Dual-expander Rocket Engine — Key to Economical Space Transportation;Beichel;Astronautics and Aeronautics,1977

2. The Next Generation Rocket Engines;Beichel;IAF-89-4219,1988

3. Performance of Advanced Engine Cycles in Future Launcher Systems;Taniguchi;IAF-87-065,1987

4. Evaluation of Innovative Rocket Engines for Single-Stage Earth-to-Orbit Vehicles;Manski;Journal of Propulsion and Power,1991

5. Variable Mixture Ratio and other Rocket Engines for Advanced Shuttles;Martin;AIAA-89-2282,1989

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multidisciplinary optimisation of bipropellant rocket engines using H2O2 as oxidiser;Aerospace Science and Technology;2018-11

2. Liquid Rocket Thrust Chambers;2004-01-01

3. Rocket Engine Nozzle Concepts;Liquid Rocket Thrust Chambers;2004-01-01

4. Advanced Rocket Nozzles;Journal of Propulsion and Power;1998-09

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