SBIR-STTR Award

Molecular Propellant Hall Effect Thruster for Enabling Multi-Mode Missions
Award last edited on: 11/8/2023

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$749,803
Award Phase
2
Solicitation Topic Code
AF211-DCSO1
Principal Investigator
Christopher Thein

Company Information

Earth Observant Inc (AKA: EOI Space)

280 Taylor Avenue Unit 200
Louisville, CO 80027
   (650) 200-3360
   N/A
   www.earthobservant.com
Location: Single
Congr. District: 14
County: San Mateo

Phase I

Contract Number: N/A
Start Date: 9/1/2021    Completed: 10/26/2022
Phase I year
2021
Phase I Amount
$1
Direct to Phase II

Phase II

Contract Number: FA8649-21-P-1574
Start Date: 9/1/2021    Completed: 10/26/2022
Phase II year
2021
Phase II Amount
$749,802
Earth Observant Inc.’s (EOI’s) Direct to Phase II work will further the development of their HET-X Hall Effect Thruster (HET) by incorporating the DoD’s desire for the use of molecular propellants in Electric Propulsion (EP) to enable multi-mode missions and to increase space asset resiliency. HETs operating directly on molecular propellants is rather novel, with little published information on compatibility or practical performance metrics. The HET-X incorporates design features not found on any other commercial HET: innovative pre-ionization technology, advanced thermal design, and a new electrical layout. These features help enable the successful testing and operation on molecular propellants. EOI intends to evaluate the HET-X against aspects of the SMC S-016 qualification process to drive design changes to enhance reliability of the hardware and provide a viable path forward for qualifying towards flight readiness. EOI will use Ascent, AF-M315E, as its main molecular propellant to conduct direct thrust measurements on the HET-X. Two key supporting subsystems to the HET-X thruster will be adapted and built so that EOI can demonstrate a path to flight to the Air Force (AF) of a HET propulsion system capable of running molecular propellants. The first subsystem would be the design and construction of a Power Processing Unit (PPU) for powering the various elements of the thruster, specifically the pre-ionizer technology and propellant flow controllers. The second subsystem would incorporate a special feed system into a more conventional Propellant Management System (PMS) for injecting molecular propellants alongside with starting and running the thruster on the control propellant of Xenon. The propulsion system that results from this work, the HET-XMP, will be a key enabling technology both commercially and for the DoD. Allowing for hybrid propulsion architectures and increased capabilities in on-orbit maneuverability.