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Dual Mode Green Monopropellant Propulsion System for Interplanetary Missions

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC21C0030
Agency Tracking Number: 193789
Amount: $749,999.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: T2
Solicitation Number: STTR_19_P2
Timeline
Solicitation Year: 2019
Award Year: 2021
Award Start Date (Proposal Award Date): 2021-01-15
Award End Date (Contract End Date): 2023-01-14
Small Business Information
4914 Moores Mill Road
Huntsville, AL 35811-1558
United States
DUNS: 799114574
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Tomas Hasanof
 (256) 851-7653
 thasanof@plasmapros.com
Business Contact
 Angela Hattaway
Phone: (256) 851-7653
Email: ahattaway@plasmapros.com
Research Institution
 Georgia Tech Research Corporation (GTRC)
 
5303
Atlanta, GA 30318-5303
United States

 Nonprofit College or University
Abstract

NASA is seeking propulsive capability for SmallSats and modular CubeSats for several lunar, interplanetary, and deep space missions. Because of their small size, CubeSats can be transported into orbit, using excess capacity of large launch vehicles ridesharing as secondary payloads. A downside of ridesharing is that satellites are often released into unfavorable trajectories/orbits that require high-precision and high-thrust chemical propulsion capability for orbital changes and other maneuvers. In the Phase I effort, a 5N low-cost ASCENT thruster was developed, and a propulsion module that included thrusters for both high-thrust and also low thrust with higher specific impulse in a dual mode propulsion system was designed. The focus of the Phase II effort is to develop a flight design for the 5N thruster and to design, fabricate, test, and deliver propellant tanks, manifold, and propulsion controller for a prototype flight unit propulsion module. The 5N thrusters will be tested to enable reaching TRL-6, and the CubeSat dual mode propulsion system will be designed, built, and tested. Georgia Tech will support the overall effort to design, build, and test a CubeSat propulsion system for performing impulsive maneuvers on small spacecraft. Georgia Tech will use its heritage CubeSat propulsion system experience and make limited changes as necessary to satisfy the unique dual mode requirements. This activity includes detailed design, fabrication, and delivery of two mechanical units: a structural test (burst) unit and a prototype field unit.

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

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