You are here

Warm Gas Generator Resistojet Micropropulsion System

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC20C0222
Agency Tracking Number: 193357
Amount: $749,849.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: Z8
Solicitation Number: SBIR_19_P2
Timeline
Solicitation Year: 2019
Award Year: 2020
Award Start Date (Proposal Award Date): 2020-07-28
Award End Date (Contract End Date): 2022-01-27
Small Business Information
2 Gregory Drive
South Burlington, VT 05403-6046
United States
DUNS: 080847279
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Michael McDevitt
 (802) 999-8211
 rmcdevitt@benchmark-space.com
Business Contact
 Michael McDevitt
Phone: (802) 999-8211
Email: rmcdevitt@benchmark-space.com
Research Institution
N/A
Abstract

In this SBIR Phase II project, Benchmark Space Systems proposes to build a resistojet micropropulsion system based on proprietarynbsp;warm gas generator technology. Results from Phase I of this project indicate that a system built around a resistojet thruster could increase specific impulse by up to 110% while remaining within the power budget of a typical CubeSat/SmallSat mission. That level of specific impulse would make the proposed propulsion system useful for Lunar and deep space missions, as well as enhancing the capabilities of low Earth orbit missions.The key advantages of the proposed system include:Unpressurized launch:nbsp;The system is launched unpressurized, and then pressurizes after a post-launch checkout. This eliminates risk associated with pressurized launches.Long Term Storage:nbsp;Since the system does not need to be pressurized until thrust is required, it can sit in a quiescent state for up to 2 years with no performance degradation or propellant lost to leakage.High Thrust:nbsp;The system is capable of operating at thrust levels up to 1N, making it viable for impulsive maneuvers.Low Cost:nbsp;The system is based around commercial-off-the-shelf components and a low-cost propellant, making it attractive for both NASA and commercial customers.This technical effort will take the concept evaluated and tested in Phase I and bring it to a flight-ready propulsion system that can be inserted into a range of upcoming commercial, DoD, or NASA technology demonstrations.

* Information listed above is at the time of submission. *

US Flag An Official Website of the United States Government