Title :
Risk reduction activities for an F-1-based advanced booster for NASA´s Space Launch System
Author :
Crocker, A.M. ; Doering, K.B. ; Cook, S.A. ; Meadows, R.G. ; Lariviere, B.W. ; Bachtel, F.D.
Author_Institution :
Dynetics, Inc., Huntsville, AL, USA
Abstract :
For NASA´s Space Launch System (SLS) Advanced Booster Engineering Demonstration and/or Risk Reduction (ABEDRR) procurement, Dynetics, Inc. and Pratt & Whitney Rocketdyne (PWR) formed a team to offer a wide-ranging set of risk reduction activities and full-scale, system-level demonstrations that support NASA´s goal of enabling competition on an affordable booster that meets the evolved capabilities of the SLS. During the ABEDRR effort, the Dynetics Team will apply state-of-the-art manufacturing and processing techniques to the heritage F-1, resulting in a low recurring cost engine while retaining the benefits of Apollo-era experience. ABEDRR will use NASA test facilities to perform full-scale F-1 gas generator and powerpack hot-fire test campaigns for engine risk reduction. Dynetics will also fabricate and test a tank assembly to verify the structural design. The Dynetics Team is partnered with NASA through Space Act Agreements (SAAs) to maximize the expertise and capabilities applied to ABEDRR.
Keywords :
aerospace engines; aerospace safety; manufacturing processes; risk management; ABEDRR; Advanced Booster Engineering Demonstration; F-1 gas generator; F-1-based advanced booster; NASA space launch system; affordable booster; engine risk reduction; manufacturing technique; powerpack hot fire test campaign; processing technique; system level demonstration; Assembly; Engines; NASA; Production; Reliability; Risk management; Testing; Aerospace Components; Aerospace Testing; Space Vehicles;
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4673-1812-9
DOI :
10.1109/AERO.2013.6496964