Small Business Innovation Research/Small Business Tech Transfer
Low-Cost High-Performance Hall Thruster Support System, Phase I
Project Introduction
Colorado Power Electronics is in the process of completing NASA SBIR contract NNC07CA12C Wide Output Range Power Processing Unit for Electric Propulsion. At the end of the project, we will have a complete brassboard PPU except for the Digital Control and Interface Unit (DCIU) and Flow Control Driver. The brassboard PPU meets the electrical requirements of the project, but the specific mass is about 20% too low compared to the first bullet of the solicitation. Preliminary results from testing a 4 kW discharge supply show that the full-power efficiency ranges from 94% to 96%. This proposal is to: (1) Determine ways to reduce the mass of the brassboard PPU (2) Evaluate the brassboard PPU to determine robustness improvements to be implemented in Phase II. (3) Determine requirements for a DCIU to be implemented in Phase II. (4) Design and build a brassboard Flow Control Driver (5) Gain experience in controlling gas flow The Flow Control Driver will be designed to control a xenon gas flow system selected by NASA. The DCIU design will be based on requirements received from NASA. The significance of this project is that it makes improvements to an innovative and promising PPU technology, moving it closer to a flight-ready product, while also facilitating NASA research with advanced flow controls.
More »
Anticipated Benefits
Non-NASA uses for the proposed idea are commercial applications for space power where low cost and high efficiency are desired. The advantages outlined for NASA applications also apply here. One specific non-NASA application is for Aerojet thrusters that are being developed for geosynchronous satellite use. Commercial non-flight applications include laboratory bench power supplies. A path to high volume sales may be achieved by using the converters refined in this SBIR for general purpose scientific equipment. The high-efficiency of the resonant converters may also lead to "green energy" applications such as solar energy power conversion. The primary market for this technology is for low-cost electric propulsion systems where Hall thrusters are likely to be used. It is anticipated that the CPE PPU will have a lower cost than state-of-the-art designs. Additionally, the high specific mass and high efficiency will reduce the overall system cost. The wide-range capabilities can help enable missions where shifts between high thrust for short-term maneuvers and high ISP for long-term operation are desirable. The wide-range capabilities also enable one PPU design to be used in a variety of different applications.
More »
Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Colorado Power Electronics, Inc. | Lead Organization |
Industry
Veteran-Owned Small Business (VOSB)
|
Fort Collins, Colorado |
Glenn Research Center
(GRC)
|
Supporting Organization | NASA Center | Cleveland, Ohio |
Primary U.S. Work Locations
-
Colorado
-
Ohio
Project Library
Share this Project
Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Colorado Power Electronics, Inc.
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Jan 2010
End: Jul 2010
Technology Maturity (TRL)
| Start: | 5 |
| Current: | 5 |
| Estimated End: | 5 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.2 Electric Space Propulsion
- TX01.2.2 Electrostatic
Target Destination
Earth
Suggest an Edit
Recommend changes and additions to this project record.
This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.