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Green Propulsion Dual Mode (GPDM) Path to FlightA team led by the NASA Marshall Space Flight Center has been developing an integrated dual mode propulsion system operating on ASCENT propellant. The small spacecraft project leveraged a wide range of NASA Space Technology Mission Directorate funding opportunities to enable the mission. The Green Propulsion Dual Model project is manifested for launch in January 2026, demonstrating a single integrated propulsion system operating off a common ASCENT propellant tank for both a catalytic combustion thruster and a set of electrospray thrusters. The objective of the flight demonstration is to mitigate risks of future, larger scale, dual mode operational systems while achieving an overall system Technology Readiness Level of 7 or higher for specific applications.
Document ID
20250008918
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
John W Dankanich
(Marshall Space Flight Center Redstone Arsenal, United States)
Nehemiah J Williams
(Marshall Space Flight Center Redstone Arsenal, United States)
Christopher G Burnside
(Marshall Space Flight Center Redstone Arsenal, United States)
Amelia R Bruno
(Massachusetts Institute of Technology Cambridge, United States)
Paulo C Lozano
(Massachusetts Institute of Technology Cambridge, United States)
E Glenn Lightsey
(Georgia Institute of Technology Atlanta, United States)
Dev Gujarathi
(Georgia Institute of Technology Atlanta, United States)
Francois Martel
(Espace Inc.)
Date Acquired
September 3, 2025
Subject Category
Propellants and Fuels
Spacecraft Propulsion and Power
Meeting Information
Meeting: 39th International Electric Propulsion Conference (IEPC)
Location: London
Country: GB
Start Date: September 14, 2025
End Date: September 19, 2025
Sponsors: Electric Rocket Propulsion Society
Funding Number(s)
WBS: 600566.10.62
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Propulsion
Technology Demonstration
ASCENT
Dual Mode
Non-Toxic Propellant
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