Modeling unburned propellant droplet distribution and velocities in plumes of small bipropellant thrusters-Reference-Cited by-同舟云学术

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Modeling unburned propellant droplet distribution and velocities in plumes of small bipropellant thrusters

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Thermophysics Conference
language:
Short-container-title:

Author:

Larin Max¹,Lumpkin III Forrest²,Stuart Phil²

Affiliation:

1. Hernandez Engineering, Inc., Houston, TX

2. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2816

Reference15 articles.

1. Rocket plume /N2O4/MMH/ impingement on aluminum surface

Cited by 6 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. Simulations and Measurements of Gas-Droplet Flows in Supersonic Jets in Vacuum;41st AIAA Thermophysics Conference;2009-06-14

2. The Effect of Reaction Control System Thruster Plume Impingement on Orion Service Module Solar Array Power Production;6th International Energy Conversion Engineering Conference (IECEC);2008-06-15

3. Mitigation of Thruster Plume Erosion of International Space Station Solar Array Coatings;Journal of Spacecraft and Rockets;2006-05

4. Kinetic Model for Simulation of Aerosol Droplets in High-Temperature Environments;Journal of Thermophysics and Heat Transfer;2004-01

5. Simulation of Particle-Based Knudsen Number Effects in Aerosols;36th AIAA Thermophysics Conference;2003-06-23

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