Aluminum combustion efficiency in solid rocket motors-Reference-Cited by-同舟云学术

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Aluminum combustion efficiency in solid rocket motors

Published:1981-01-12 Issue: Volume: Page:
ISSN:
Container-title:19th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HERMSEN R.¹

Affiliation:

1. United Technologies Corp., Chemical Systems Div., Sunnyvale, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-38

Reference15 articles.

1. Crowe, C. T., R. Dunlap, e t al. "High Perfomance Nozzles for Solid Propellant Rocket Motors," UTC Final Report 2025FR, NASA Contract No. NAS-7-178, UTC, 25February 1965.

2. Performance of solid propellants containing metal additives

3. Pokhil, P. F., Belyayev, e t al. "Combustion of Powdered Metals i n Active Media," FTD-MT24-5551-73, Foreign Technology Division.

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1. Modeling of Micro Aluminum Particle Flames Using Particle Burning Time;Combustion Science and Technology;2024-07-29

2. Influence of Aluminum Content and Agglomerates Initial Velocity on Erosion in Solid Rocket Motor;Journal of Energy Resources Technology;2024-07-26

3. Factors in Condensate Product Particle Size During Aluminized Propellant Combustion;AIAA Journal;2023-08

4. Detecting agglomeration patterns on solid propellant surface via a new curvature-based multiscale method;Acta Astronautica;2023-05

5. Mechanical Erosion Investigation in Solid Rocket Motor Nozzle Through Droplet Breakup and Surface Tension Influence;Journal of Energy Resources Technology;2023-03-28

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