SBIR/STTR Research Award

Fail-safe Cold Cathode Ionizer

Award identifier 47e8e17266341617d1f6b18b8ad9e3bbc2213d123c4b83f98fb3ec9051d44ff1Awarding agency National Aeronautics and Space Administration

Award amount

$124,027

Program and phase

SBIR · Phase I

Award year

2021

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
PHYSICAL SCIENCES INC.
Proposal award date
2021-05-05
Contract end date
2021-11-19
UEI
RMG1AZ1ZH8Q7
Solicitation number
SBIR_21_P1
Topic code
S1

Research 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.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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