LOX/methane and LOX/kerosene high thrust engine trade-off-Reference-Cited by-同舟云学术

LOX/methane and LOX/kerosene high thrust engine trade-off

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Pempie Pascal¹,Froehlich Thomas¹,Vernin Hilda²

Affiliation:

1. CNES Launcher Directorate, Evry, France

2. Ligeron S. A., Saint-Aubin, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3542

Reference20 articles.

1. TJ. Healy jr. Shuttle liquid Fly back Booster Configuration Options. 1998JANNAFJPM.

2. R.M. Ryan. Booster Main Engine Selection criteria for Liquid Fly Back Booster TM 208-106.

3. H. Grallert, G. Reinbold.OptimizedLiquidRy BackBoosterconcept withAriane 5core stage. AIAA 2001-1845.

4. LA. Klepikov, B.I. Kartagin, V.K. Chavanov. The new Generation of Rocket Engines, Operating by Ecologically Safe Propellant "Liquid OxygenandLNG". IAF 17-5-103.

Cited by 17 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. Analysis of bubble dynamics and thermal destratification induced by gas bubbles in cylindrical liquid storage tanks;Thermal Science and Engineering Progress;2022-12

2. Rankine Vortex Suppression in Tanks with Conical Base: A Numerical Investigation;Journal of Spacecraft and Rockets;2021-03

3. The precursor shock wave and flame propagation enhancement by CO2 injection in a methane-oxygen mixture;Fuel;2021-01

4. Time-resolved flow field and thermal loads in a single-element GOx/GCH4 rocket combustor;International Journal of Heat and Mass Transfer;2019-11

5. Numerical investigation on the film cooling performance in a multi-elements splash platelet injector;Acta Astronautica;2018-11