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E-field Instrument for CubeSats

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9453-12-M-0057
Agency Tracking Number: F112-083-2386
Amount: $149,996.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: AF112-083
Solicitation Number: 2011.2
Timeline
Solicitation Year: 2011
Award Year: 2012
Award Start Date (Proposal Award Date): 2011-11-14
Award End Date (Contract End Date): N/A
Small Business Information
5777 Central Avenue, Suite 221
Boulder, CO -
United States
DUNS: 601975803
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Geoffrey Crowley
 President/Chief Scientist
 (210) 834-3475
 gcrowley@astraspace.net
Business Contact
 Geoffrey Crowley
Title: President/Chief Scientist
Phone: (210) 834-3475
Email: 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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