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Space Plug-and-Play Compatible Wireless Avionics

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W91CRB-10-C-0192
Agency Tracking Number: 08SB2-0905
Amount: $750,000.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: SB082-060
Solicitation Number: 2008.2
Timeline
Solicitation Year: 2008
Award Year: 2010
Award Start Date (Proposal Award Date): 2010-09-29
Award End Date (Contract End Date): 2012-09-28
Small Business Information
15400 Calhoun Drive Suite 400
Rockville, MD -
United States
DUNS: 161911532
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Wendy Nicholas
 Senior Electrical Enginee
 (301) 294-5273
 wnicholas@i-a-i.com
Business Contact
 Mark James
Title: Director, Contracts and P
Phone: (301) 294-5221
Email: mjames@i-a-i.com
Research Institution
N/A
Abstract

Weight, reliability and cost are important factors in the design of launch vehicles. The weight of wire harnesses, connectors and stage separation devices can make up a significant portion of the launch vehicle. Qualification of these components adds additional cost and schedule delays. Harnesses and connectors are subject to operational concerns such as wire crosses, insulation damage due to thermal or vibration effects, and limited mate/de-mate cycles for connectors. Design considerations such as minimum harness bend radii, separation forces required for connectors, and securing harnesses to withstand vibration add to the development and qualification costs. Furthermore, the variable nature of payloads imposes a wide variety of interface requirements to the launch vehicle. To address this need, Intelligent Automation Incorporated (IAI) is developing an Ultra Wideband (UWB) radio with a redundant Power Line Communications (PLC) link that can replace communication harnessing in any Ethernet based launch vehicle. The anticipated result of the Phase II effort is a prototype system, composed of redundant UWB radio and PLC links, that has operated successfully during flight simulation on a launch vehicle test bed.

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

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