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RS-84 EngineThe RS-84 is the first reusable hydrocarbon staged combustion liquid rocket engine. This engine is being developed to meet NASA s crew safety goals with a highly reliable and low cost main engine as a part of the NASA Space Launch Initiative program for the next generation reusable launch system. The NASA-MSFC and Rocketdyne team brings over 50 years of successful rocket engine development experience to meet the challenges of this new program. This team s extensive design database has been anchored with almost five decades of hydrocarbon rocket engine development and flight operations experience including Delta, Atlas, and Saturn vehicles and nearly three decades of successfully operating the world s only reusable pump-fed rocket engine, the Space Shuttle Main Engine. The team also fully benefits from the proven and experienced engineering staffs that recently completed the successful MC-1 FASTRAC , XRS-2200, and RS-68 engine development programs and the ongoing IPD and RS-76 technology development. Advances in integrated parametric design and analysis tools, advanced materials knowledge base, and state-of-the-art fabrication processes anchored and refined during the recent engine development programs are already being used by the team to design this engine.
Document ID
20030066142
Document Type
Conference Paper
Authors
Stegman, E. (Boeing Co. Canoga Park, CA, United States)
Date Acquired
August 21, 2013
Publication Date
March 20, 2003
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Joint Propulsion Conference(Huntsville, AL)
Funding Number(s)
CONTRACT_GRANT: NAS8-01107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.