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Orion Exploration Flight Test-1 (EFT-1) Absolute Navigation PerformanceThe Orion vehicle, being design to take men back to the Moon and beyond, successfully completed its first flight test, EFT-1 (Exploration Flight Test-1), on December 5th, 2014. The main objective of the test was to demonstrate the capability of re-enter into the Earth's atmosphere and safely splash-down into the pacific ocean. This un-crewed mission completes two orbits around Earth, the second of which is highly elliptical with an apogee of approximately 5908 km, higher than any vehicle designed for humans has been since the Apollo program. The trajectory was designed in order to test a high-energy re-entry similar to those crews will undergo during lunar missions. The mission overview is shown in Figure 1. The objective of this paper is to document the performance of the absolute navigation system during EFT-1 and to present its design.
Document ID
20150004541
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Zanetti, Renato
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
April 8, 2015
Publication Date
August 9, 2015
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Launch Vehicles And Launch Operations
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-33060
Report Number: JSC-CN-33060
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Vail, CO
Country: United States
Start Date: August 9, 2015
End Date: August 13, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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