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A Practical, Affordable Cryogenic Propellant Depot Based on ULA's Flight ExperienceMankind is embarking on the next step in the journey of human exploration. We are returning to the moon and eventually moving to Mars and beyond. The current Exploration architecture seeks a balance between the need for a robust infrastructure on the lunar surface, and the performance limitations of Ares I and V. The ability to refuel or top-off propellant tanks from orbital propellant depots offers NASA the opportunity to cost effectively and reliably satisfy these opposing requirements. The ability to cache large orbital quantities of propellant is also an enabling capability for missions to Mars and beyond. This paper describes an option for a propellant depot that enables orbital refueling supporting Exploration, national security, science and other space endeavors. This proposed concept is launched using a single EELV medium class rocket and thus does not require any orbital assembly. The propellant depot provides cryogenic propellant storage that utilizes flight proven technologies augmented with technologies currently under development. The propellant depot system, propellant management, flight experience, and key technologies are also discussed. Options for refueling the propellant depot along with an overview of Exploration architecture impacts are also presented.
Document ID
20130010201
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Kutter, Bernard F.
(United Launch Alliance Denver, CO, United States)
Zegler, Frank
(United Launch Alliance Denver, CO, United States)
O'Neil, Gary
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Pitchford, Brian
(Analex Corp. United States)
Date Acquired
August 27, 2013
Publication Date
September 9, 2008
Subject Category
Astronautics (General)
Report/Patent Number
KSC-2008-140
Report Number: KSC-2008-140
Meeting Information
Meeting: AIAA Space 2008
Location: San Diego, CA
Country: United States
Start Date: September 9, 2008
End Date: September 11, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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