E-field Instrument for CubeSats

Award Information
Agency:
Department of Defense
Branch
n/a
Amount:
$149,996.00
Award Year:
2012
Program:
SBIR
Phase:
Phase I
Contract:
FA9453-12-M-0057
Award Id:
n/a
Agency Tracking Number:
F112-083-2386
Solicitation Year:
2011
Solicitation Topic Code:
AF112-083
Solicitation Number:
2011.2
Small Business Information
5777 Central Avenue, Suite 221, Boulder, CO, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
601975803
Principal Investigator:
Geoffrey Crowley
President/Chief Scientist
(210) 834-3475
gcrowley@astraspace.net
Business Contact:
Geoffrey Crowley
President/Chief Scientist
(210) 834-3475
gcrowley@astraspace.net
Research Institution:
Stub




Abstract
ABSTRACT: The Air Force and other DoD components require accurate knowledge of the ionospheric environment to understand and predict its impacts on vital radio-based systems, including communications, navigation, and surveillance systems. In response to the STTR Topic AF112-083 we propose to develop a conceptual design for a miniature, low-cost, lightweight, high sensitivity electric field instrument using the double probe technique to provide in-situ measurements of ionospheric electric fields. Our focus will be on developing a new electric field sensor that meets or exceeds the performance of SSIES, yet has significantly smaller mass and power requirements such that it can fly on CubeSats or nano-satellites. The new design will also be Space Plug-and-Play Avionics (SPA) compatible. The name of the new instrument is DIME (Double-probe Instrumentation for Measuring E-fields). DIME will draw heavily from the lessons learned in developing the electric field instrument for the DICE mission. It also benefits from ASTRA"s experience with Space Plug-n-Play Avionics (SPA). BENEFIT: The DIME (Double-probe Instrumentation for Measuring E-fields) sensor is a new electric field sensor that meets or exceeds the performance of SSIES, yet has significantly smaller mass and power requirements such that it can fly on CubeSats or nano-satellites. The new design will also be Space Plug-and-Play Avionics (SPA) compatible, so it can contribute to the efforts that are underway to develop complete PnP satellite systems built on a SPA backbone using SPA components. It is suitable for mass-production, and is expected to populate the fleets of CubeSats that are expected to fly in the near-future. Small size and low operating power enable the DIME sensor to fly on any spacecraft from the smallest (CubeSat) to the largest.

* information listed above is at the time of submission.

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