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Development of Novel Green Propellant Dual-Mode Thrusters

Completed TRL 5 (started at 4, targeting 6)

Description

Project Objective  

Igneon Aerospace (Hyperion) is addressing the relatively limited market availability of low-toxicity thrusters by developing small spacecraft-scale thrusters which can use multiple blends of the the Advanced Space Craft Energetic Non-Toxic (ASCENT) family of ionic liquid propellants.

Project Description 

Igneon Aerospace (formerly Hyperion) aims to develop and demonstrate a new generation of low-toxicity monopropellant thrusters that use ASCENT and its blends (e.g., DM-4) developed by the Air Force Research Laboratory (AFRL). The goal is to provide affordable, high-performance, and both low-cost and relatively easily manufacturable thruster products for small spacecraft.

Goals of this project include:

Project Results and Conclusions 
 

With FY25, Igneon has successfully designed both the 0.2-N and the 22-N ASCENT thruster per the Cooperative Agreement Notice (CAN) with NASA MSFC. The 0.2-N thruster components were successfully manufactured, assembled, and subsequently performed acceptance testing with ASCENT, estimating a move from TRL-4 to TRL-6. Hyperion has recently overcome challenges with acquisition of the DM-4 propellant blend as well as longer than anticipated lead times for the manufacturing of the 22-N thruster. This has led to the need for an extension of this effort. Igneon hopes to complete a 0.2-N thruster test campaign with DM-4 as well as an eventual assembly and test of the 22-N thruster.

Benefits

Project benefits include increasing thruster options for small spacecraft which use non-toxic propellants in small and larger thruster classes. Additional benefits include reduction in cost and overall lead time of manufacturing small satellite non-toxic thrusters. Also, the thrusters produced by Igneon will demonstrate use for various blends of ASCENT; this will allow for a wider range of applications for dual-mode (chemical and electrospray) propulsion systems and mission classes.

Details

Technology areaPropulsion Systems
ProgramCenter Independent Research & Development: MSFC IRAD (MSFC IRAD)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2025-01-01
End date2026-01-31

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