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Space Launch System Launch Window and Day of Launch ProcessesLunar missions benefit from varying the launch azimuth as a function of launch time to allow longer launch windows with minimum performance impacts. This variable azimuth approach allows the vehicle to track the Moon’s apparent motion due to Earth’s rotation . The Space Launch System (SLS) Block 1 vehicle design requires the mission to launch into an elliptical parking orbit to provide sufficient energy to insert Orion into a trans-lunar trajectory. The primary benefit of varying the launch azimuth, and as a result the parking orbit inclination, allows the SLS Interim Cryogenic Propulsion Stage (ICPS) to perform its Trans-Lunar Injection (TLI) burn closer to perigee and take advantage of performing a burn in a location where the burn will primarily raise apogee.
Document ID
20205001580
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
A. S. Craig
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
N. Ahmad
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Date Acquired
April 30, 2020
Subject Category
Launch Vehicles And Launch Operations
Meeting Information
Meeting: 2020 AAS/AIAA Astrodynamics Specialist Conference
Location: Virtual
Country: US
Start Date: August 9, 2020
End Date: August 13, 2020
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: 585777.02.20.04.02.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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