Dual fuel solar thermal propulsion - Computational assessment of nozzle performance-Reference-Cited by-同舟云学术

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Dual fuel solar thermal propulsion - Computational assessment of nozzle performance

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Landrum D.¹,Beard Robert¹

Affiliation:

1. Alabama, Univ., Huntsville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3217

Reference21 articles.

1. 4Grisnik, S. P., Smith, T. A., and Saltz, L. E. "Experimental Studyof LowReynolds NumberNozzles,"NASATM-89858 (AIAA Paper 87-0992),May 1987.

2. 5CFDResearchCorporation,Huntsvflle, AL, 1993.

Cited by 1 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. Effects of test chamber ambient pressure on the performance of hydrogen thrusters for solar thermal rockets;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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