SBIR/STTR Research Award

A Universal High Efficiency Modular Discharge Over a Wide Input/Output Voltage Range for Hall Thruster Power Processing Unit

Award identifier 2fcf43c19ae27e4f1e80ad5644c4c343b3939c59db3b0a58b7f8fae296690182Awarding agency National Aeronautics and Space Administration

Award amount

$125,000

Program and phase

SBIR · Phase I

Award year

2017

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BUSEK CO., INC.
Proposal award date
2017-06-09
Contract end date
2017-12-08
UEI
SATYSBWG3FL7
Solicitation number
Not reported
Topic code
S3.03

Research abstract

Busek proposes a novel, universal, modular, 2.5kW discharge converter for Hall Effect thruster (HET) Power Processing Unit (PPU). The unique advantages of the proposed system include:(1) a wide input voltage range (28V to 100V) with a wide output voltage (150V to 400V) while maintaining high efficiency operation. Therefore, it provides a universal solution for aerospace systems with different bus voltages. (2) this modular converter will be capable of input-parallel output-series (IPOS) operation to support higher output voltage (800V-1200V or higher) and input-parallel output-parallel (IPOP) operation to support higher output power (20kW or higher). An intelligent "plug-n-play" power sharing and voltage balancing control is proposed to support the IPOS and IPOP operations. (3) the proposed converter adopts a soft-switching DC/DC topology using the advanced GaN power MOSFETs to enable high efficiency with high switching frequency operation, which leads to significant size reduction of magnetics and other passive components to push for high power density design. The targeting power density for single module is more than 1kW/kg. The Phase I effort includes design and analysis of modular discharge converter with the GaN power MOSFETs and the "plug-n-play" power sharing and voltage balancing control system to support IPOS and IPOP operation. The bread board will use COTS EEE parts. Its testing will validate the performance over the wide input/output voltage range. Two modules will verify IPOS and IPOP operation. The initial system integration test with Busek HET will also be conducted. In Phase II we will fully characterize the breadboard discharge converter with a thruster and develop a proto-flight brass-board level unit with multiple discharger modules using GaN devices. At the conclusion of Phase II we will build and deliver several discharger modules to NASA for additional characterization testing.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

248 SBIR/STTR records share this UEI (1988–2026). Reported award amounts total $87,675,405. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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