SBIR/STTR Research Award

Small TEnuous Plasma Heliophysics Electric field Instrument (STEPHEI)

Award identifier c96b501f54df71a4bdfc2bb5673c111504a66330c797591fb2ff7b40895579f9Awarding agency National Aeronautics and Space Administration

Award amount

$156,466

Program and phase

SBIR · Phase I

Award year

2023

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ATMOSPHERIC & SPACE TECHNOLOGY RESEARCH ASSOCIATES LLC
Proposal award date
2023-07-27
Contract end date
2024-02-02
UEI
DRYZNRMCBKL6
Solicitation number
SBIR_23_P1
Topic code
S14

Research abstract

Much of the outstanding physics yet to be learned about the coupling of the magnetosphere-ionosphere (M-I) system resides in the small- and mesoscale structures of the aurora, field aligned currents, plasma convective motions, and wave activity. Untangling these spatial and temporal structures with in situ measurements will require a constellation of spacecraft. For cost-effectiveness, such a constellation would consist of CubeSats. To study M-I coupling, one of the essential measurements these CubeSat will need to make is of the DC electric field. The electric field plays a crucial role in M-I coupling from driving convective drifts in the magnetosphere and ionosphere, Joule heating, Poynting flux, waves, and auroral particle precipitation. The environment on the magnetospheric side of these processes is the tenuous plasmas of the earthward plasma sheet, plasma sheet boundary layer, ring current, and auroral zone. In such environments, the sunlit electric field sensors are surrounded by high plasma sheath impedance which causes large errors on the measurement. To reduce the sheath impedance, a bias current is driven from the spacecraft to the sensors. This current is large relative to the plasma thermal current to CubeSatrsquo;s small surface area, causing the CubeSat to charge to large potentials, contaminating the measurement. By effectively increasing the spacecraft surface area of a CubeSat, enough thermal plasma current can be collected to offset the effect of the bias current. STEPHEI, the Small TEnuous Plasma Heliophysics Electric field Instrument, is an electric field double probe for CubeSats in tenuous plasmas with a deployable electron collector that will prevent the spacecraft charging. The electron collector consists of a metallized polymer sheath deployed along either the sensor booms or on its own boom. STEPHEI will allow the measurements to be made that are needed to address fundamental problems in M-I coupling.nbsp;

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

56 SBIR/STTR records share this UEI (2007–2023). Reported award amounts total $18,884,787. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Commerce

Agency intelligence

National Aeronautics and Space Administration

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