Model for steady-state combustion of unimodal composite solid propellants-Reference-Cited by-同舟云学术

Model for steady-state combustion of unimodal composite solid propellants

Published:1978-01-16 Issue: Volume: Page:
ISSN:
Container-title:16th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

KING M.¹

Affiliation:

1. Atlantic Research Corp., Alexandria, Va.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1978-216

Reference6 articles.

1. Combustion Tailoring Criteria For Solid Propellants, Lockheed Propulsion Company, Lockheed Report 835F, AFRPL-TR-69-190,May, 1969. 4. Waesche,R.H.W., and Wenograd,J. "Calculation

2. of Solid Propellant Burning Rates From Condenscd-phase DecompositionKinetics,'I AIAA 7th Aerospace Sciences Meeting, January, 1969, AIM Paper 69-145. Also, United Aircraft Final Report on Research Investigation of the Decomposition of Composite Solid Propellants,Report H910457-37, Sept., 1969. 5. Burke,S.P., and Sehumann,T.E.W. "Diffusion

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