Enhanced large solid rocket motor understanding through performance margin testing - RSRM five-segment engineering test motor (ETM-3)

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Huppi, Hal ^a   Tobias, Mark ^a   Seiler, James ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN AND ANALYSIS; DEVELOPMENT PROGRAMS; NORMAL OPERATIONS; REPLACEMENT MATERIALS; REUSABLE SOLID ROCKET MOTORS; SOLID ROCKET MOTORS; SPACE SHUTTLE PROGRAMS; TECHNICAL PERSONNEL;

DESIGN; NASA; PROPULSION; ROCKET ENGINES; SPACE SHUTTLES;

ROCKETS;

EID: 84897756056     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Donald R. Sauvageau, Bob Ess, and Joe Craft, "Achieving Shuttle ATO Using Five-Segment Booster (FSB), " AIAA 2003-5127.
2. Mark Tobias, Donald R. Sauvageau, Mark Hines, and Norman L. Geiser, "Five-Segment Booster Abort-to-Orbit Studies, " AIAA 2002-3759.
3. James A. Furfaro, Brian Laubacher, and Donald R. Sauvageau, "Five-Segment Booster (FSB) Phase A Study Results, " presented at JANNAF Propulsion Meeting in Salt Lake City July 12-13, 2001.
4. Donald R. Sauvageau, "Achieving Space Shuttle ATO Using the Five-Segment Booster (FSB), " AIAA 2001-3413.
5. Donald R. Sauvageau, Hal D. Huppi, "Shuttle Upgrade Using Five-Segment Booster (FSB), " AIAA 2000-5070.
6. Brian W. Rex, Quinn Wang, and Daron Isaac, "An Automated Fluid-Structural Interaction Analysis of a Large Segmented Solid Rocket Motor, " AIAA 2003-4507.
7. James A. Furfaro, "Erosive Burning Study Utilizing Ultrasonic Measurement Techniques, " AIAA 2003-4806.
8. Rashid A. Ahmad, Robert A. Morstadt, Andrew M. Eaton, "RSRM and ETM-3 Internal Flow Simulations and Comparisons, " AIAA 2003-5104.
9. Qunzhen Wang, "Development of Erosive Burning Models for CFD Predictions of Solid Rocket Motor Internal Environments, " AIAA 2003-4809.