Low temperature liquid propellant - An alternative propulsion source for space exploration-Reference-Cited by-同舟云学术

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Low temperature liquid propellant - An alternative propulsion source for space exploration

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Shahnam Mehrdad¹,McAllister Andrew¹,Stechman Carl¹,Nejad Abdi¹,Carlson Ron²,Guernsey Carl²

Affiliation:

1. Kaiser Marquardt, Van Nuys, CA

2. JPL, Pasadena, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2463

Reference7 articles.

1. Structure of sprays generated by unlike doublet injectors

2. 4- (A) oxidizer valve switch on (Et) oxidizer valve open (C) oxidizer valve fully dpen (D) chamberpressurerise dueto ignition I 1.5 -4

3. - _._._._*`- chamber pressure 1.905 1.91 1.915 Elapsedtime, set-2$1 H -4 g - 73 -4 2 -8

4. chamber pressure -700 -0

Cited by 2 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. Small Batch Synthesis of Mixed Oxides of Nitrogen;AIAA Propulsion and Energy 2020 Forum;2020-08-17

2. Chemical Propulsion for Outer Planet Exploration;AIAA Propulsion and Energy 2019 Forum;2019-08-16

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