A Multi-Mission, Integrated Avionics Module for Short-Duration MDA Applications

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$69,942.00
Award Year:
2002
Program:
STTR
Phase:
Phase I
Contract:
F29601-02-C-0248
Award Id:
56101
Agency Tracking Number:
02-0069T
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
520 Huntmar Park Drive, Herndon, VA, 20170
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
605603984
Principal Investigator:
ScottMcDermott
Senior Engineer
(703) 709-2240
scott@aeroastro.com
Business Contact:
DavidGoldstein
VP, Business Development
(617) 451-8630
david@aeroastro.com
Research Institute:
University of Alabama In Huntsville
Gary L Workman
203 Sparkman Drive
Huntsville, AL, 35899
(256) 824-6578
Nonprofit college or university
Abstract
"For missions deploying maneuverable vehicles for Boost-Phase and Space-Based Intercept, as well as refueling and resupply for SBIRS Low and Space-Based Laser, MDA requires a compact, highly versatile avionics core with a design that can be reused at verylow cost for a variety of missions. Leveraging previous work, AeroAstro and the University of Alabama Huntsville propose to develop a flexible, capable, and inexpensive multi-mission core avionics module that will serve as a common core for a variety ofshort-duration missions. This core will be highly flexible and re-useable for multiple mission designs. While varying MDA applications require unique spacecraft solutions, there are many similarities in basic avionics requirements that can be leveragedfor a significant overall cost savings.Conventional design is heavily biased toward long-lifetime, solar-powered missions with high power and complex control schemes. Similarly, conventional design is effected in two discrete parts: a payload system, and a support system ("bus"). Althoughthis functional partitioning of tasks should provide a foundation for efficient system design, the physical constraints inherent in spacecraft often force a structural interdependence that minimizes these advantages. This project will eliminate thereliance on a custom bus approach. AeroAstro and UAH believe there is a strong demand for this low-cost, flexible spacecraft electronics module, both within the government and in non-government organizations. The types of applications this development will benefit can be broken up intothree main categories. The first category includes technology demonstration missions. These missions are generally budget limited and require only a limited time in space to demonstrate the performance of the device - these two factors make technologydemonstration missions perfect candidates for the proposed technology. The second category includes Space Station deployables. There are a number of experiments for which the Space Station is an ideal launch platform but a poor e

* information listed above is at the time of submission.

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