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Fail-safe Cold Cathode Ionizer

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC21C0112
Agency Tracking Number: 211579
Amount: $124,027.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: S1
Solicitation Number: SBIR_21_P1
Timeline
Solicitation Year: 2021
Award Year: 2021
Award Start Date (Proposal Award Date): 2021-05-05
Award End Date (Contract End Date): 2021-11-19
Small Business Information
20 New England Business Center
Andover, MA 01810-1077
United States
DUNS: 073800062
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Jonathan Rameau
 (978) 738-8265
 jrameau@psicorp.com
Business Contact
 Michael Healy
Title: mhealy
Phone: (978) 738-8107
Email: mhealy@psicorp.com
Research Institution
N/A
Abstract

NASA has expressed a need for advanced neutral particle ionizers to enable the next-generation of neutral particle detectors such as mass spectrometers for the study of Earth-Sun interactions and planetary atmospheres. To fulfil this need, Physical Sciences Inc. (PSI) proposes to develop a fail-safe field emission-based cold cathode ionizer for use in space-based instrumentation.nbsp;The cold cathode ionizer features ultra-low electron extraction voltages down to 2 V, emission current densities up to A/cm2 across mm2 emission surfaces, instantaneous switching and negligible thermal load. A unique property of PSIrsquo;s proposed cold cathode ionizer is its extreme resistance to the most common failure modes associated with field emission devices. The device is designed with recovery from mechanical and thermal shock as well as resilience against exposure to debris or contamination that might be encountered during its service lifetime. The slow degradation of materials and surfaces encountered in space are inherently compensated for in the design.nbsp;In Phase I of the program, PSI will demonstrate the principle of the ionizer, raising its technology readiness level (TRL) from 2 to 3. The cathode fabrication process will be developed and cathodes integrated into a demonstration device for evaluation of critical components and operating parameters. Phase I will culminate in production of a detailed preliminary design for a flight-worthy prototype ionizer. In Phase II, ionizer requirements and capabilities will be finalized. A flight-worthy prototype will be constructed and evaluated. The Phase II program will be exited with the ionizer at TRL 6 and with the prototype delivered to NASA for further evaluation. Following Phase II, PSI will work with NASA to identify opportunities to incorporate the new enabling technology into instrumentation for upcoming missions such as Geospace Dynamics Coupling (GDC), and opportunities for NASA-sponsored technology demonstration flights.

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

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