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Cryogenic Hydrogen Oxygen Propulsion System for Planetary Science MissionsA Cryogenic Hydrogen Oxygen Propulsion System (CHOPS) that uses liquid hydrogen (LH2) and liquid oxygen (LO2) propellants can dramatically enhance NASA's ability to explore the solar system due to their superior specific impulse (Isp) capability. Although these cryogenic propellants can be challenging to manage and store, they allow significant mass advantages over traditional hypergolic propulsion systems and are therefore enabling for many planetary science missions. New cryogenic storage techniques such as subcooling, advanced insulation, low thermal conductivity structures allow for the long term storage and use of cryogenic propellants for solar system exploration and hence allow NASA to deliver more payloads to targets of interest, launch on smaller and less expensive launch vehicles, or both.
Document ID
20200000753
Acquisition Source
Goddard Space Flight Center
Document Type
Poster
Authors
Mustafi, Shouvanik
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Purves, Lloyd
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Nixon, Conor
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Douglawi, Alber
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hedayat, Ali
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Simpson, Steven
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
February 5, 2020
Publication Date
February 3, 2020
Subject Category
Spacecraft Propulsion And Power
Engineering (General)
Report/Patent Number
GSFC-E-DAA-TN77348
Report Number: GSFC-E-DAA-TN77348
Meeting Information
Meeting: Outer Planets Assessment Group (OPAG)
Location: Houston, TX
Country: United States
Start Date: February 3, 2020
End Date: February 4, 2020
Sponsors: Lunar and Planetary Institute (LPI)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
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