SBIR/STTR Research Award

Propellant Storage and Distribution System Based on Textured Ceramic Valves for Xenon Electric Propulsion Systems

Award identifier 3757ec59570d0a38e0d95ce68020e97c37059f46c4b2ead47d77cbb627a13dd5Awarding agency National Aeronautics and Space Administration

Award amount

$124,997

Program and phase

STTR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
QORTEK INC
Proposal award date
2019-08-19
Contract end date
2020-09-18
UEI
TLD8L3APDZM3
Solicitation number
STTR_19_P1
Topic code
T2

Research abstract

QorTek is proposing a remarkable design of a subcompact solid-state (textured ceramic) actuated Xenon flow control systems that feeds a heaterless cathode assembly. Eliminating both pressure regulator nbsp;and solenoid actuation, the revolutionary solid-state design introduces true linear response at higher bandwidth than anything presently available to the space community as to enable extremely precise flow rate control. One fill and drain port and three precision gas flow outputs will be provided to enable operation of an ion thruster, two of which will be used to enable operation of a Hall thruster. The new flow control system is capable of scaling such that it can fit as a universal assembly to the boss of a propellant storage tank. The pre- integrated electronic controller and power supply sub-system can accept external commands to set arbitrary flow rate profiles on each channel. This capability will enable both heaterless and heater-equipped hollow cathodes to be started and operated without adding additional components to the cathode gas lines. The innovation relies on our advances in textured ceramic actuation as to enable very fast valving operation. MHz pulse-width modulation allows users to set arbitrarily defined flow rates characteristics with extremely high precision. The availability of our system will greatly simplify the integration of electric propulsion systems onto small, medium, and large spacecraft and satellites due to its large size, weight, planform, and power reductions over all existing solutions. nbsp;Its relatively low cost will encourage spacecraft designers to adopt the technology. Although the initial system is targeted toward NASA Class D missions, the extremely high reliability of our solid-state drive technology will enable all many NASA and commercial space missions to benefit from its use.

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.

Research funding history

136 SBIR/STTR records share this UEI (1996–2025). Reported award amounts total $62,777,779. 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

Agency intelligence

National Aeronautics and Space Administration

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