Modern SRM ignition transient modeling. I - Introduction and physical models-Reference-Cited by-同舟云学术

Modern SRM ignition transient modeling. I - Introduction and physical models

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Salita Mark¹

Affiliation:

1. TRW Space and Missile Systems Div., San Bernardino, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3443

Reference37 articles.

1. Lundgreen,R."ModernSRMIgnitionTransient Modeling(Part 2):AnalysesRoutinelyConductedat AlliantTechsystems",AIAA2001-3444,37thJoint PropulsionConference (SaltLakeCity),7/2001.

2. Graham,Robert,"ModernSRMIgnitionTransient Modeling(Part 4):SBAS",AIAA2001-3446,37thJoint PropulsionConference (SaltLakeCity),7/2001.

3. Wang,J.C.T."ModernSRMIgnitionTransient Modeling(Part 5):",AIAA2001-3447,37thJoint PropulsionConference (SaltLakeCity),7/2001.

4. Salita,M."Volume-FillingCalculationsforIgnition Transients",Thiokolmemo 2814-80-M128,10/17/80.

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