A Flight Dynamics Perspective of the Orion Pad Abort One Flight Test

Idicula, Jinu T. and Hayes, Peggy S. and Stillwater, Ryan A. and Yates, Max W. (2009) A Flight Dynamics Perspective of the Orion Pad Abort One Flight Test.

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Abstract

The Orion Crew Exploration Vehicle is America's next generation of human rated spacecraft. The Orion Launch Abort System will take the astronauts away from the exploration vehicle in the event of an aborted launch. The pad abort mode of the Launch Abort System will be flight-tested in 2009 from the White Sands Missile Range in New Mexico. This paper examines some of the efforts currently underway at the NASA Dryden Flight Research Center by the Controls & Dynamics group in preparation for the flight test. The concept of operation for the pad abort flight is presented along with an overview of the guidance, control and navigation systems. Preparations for the flight test, such as hardware testing and development of the real-time displays, are examined. The results from the validation and verification efforts for the aerodynamic and atmospheric models are shown along with Monte Carlo analysis results.

EPrint Type:	Other
Subjects:	(01 - 09) Aeronautics: (05) Aircraft Design, Testing And Performance
ID Code:	2034
Deposited On:	24 August 2009
Additional Information:	11 pages. Presented at the AIAA Atmospheric Flight Mechanics Conference, Chicago, Illinois, August 10-13, 2009.