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Propulsion Overview of the Orion Pad Abort 1 (PA-1) Flight-Test VehicleThe NASA Orion Flight Test Office was tasked with conducting a series of flight tests in several launch abort scenarios to certify that the Orion Launch Abort System is capable of delivering astronauts aboard the Orion Crew Module to a safe environment, away from a failed booster. The first of this series was the Orion Pad Abort 1 Flight-Test Vehicle, which was successfully flown on May 6, 2010 at the White Sands Missile Range in New Mexico. This presentation provides a concise overview of the three propulsive subsystems used on the Pad Abort 1 Flight-Test Vehicle. Although the Constellation program has been cancelled and the operational role of the Orion spacecraft has significantly evolved, lessons learned from Pad Abort 1 could certainly contribute to the vehicle architecture of many future human-rated space launch vehicles
Document ID
20170011295
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Jones, Daniel S.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
November 27, 2017
Publication Date
June 5, 2013
Subject Category
Space Transportation And Safety
Launch Vehicles And Launch Operations
Report/Patent Number
AFRC-E-DAA-TN8681
Report Number: AFRC-E-DAA-TN8681
Meeting Information
Meeting: NASA Dryden Brown-Bag Session 2013
Location: Edwards, CA
Country: United States
Start Date: June 5, 2013
End Date: June 9, 2013
Sponsors: NASA Armstrong Flight Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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