SCOUT: A Modular, Multi-Mission Spacecraft Architecture for High Capability Rapid Access to Space

Award Information
Agency:
Department of Defense
Branch
Defense Advanced Research Projects Agency
Amount:
$748,745.00
Award Year:
2004
Program:
SBIR
Phase:
Phase II
Contract:
W31P4Q-04-C-R071
Agency Tracking Number:
02SB2-0396
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
AEROASTRO, INC.
20145 Ashbrook Place, Ashburn, VA, 20147
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
605603984
Principal Investigator:
Scott McDermott
Principal Investigator
(703) 723-9800
scott.mcdermott@aeroastro.com
Business Contact:
Mike Conley
VP, Programs
(703) 723-9800
mike.conley@aeroastro.com
Research Institution:
n/a
Abstract
In this Phase II effort AeroAstro will refine and focus the rapid response, modular spacecraft architecture development, SCOUT, begun in Phase I. In Phase I AeroAstro identified several key, enabling technologies that must be matured to realize a responsive space military asset. Plug-and-Sense Connectivity - a software architecture that detects attached modules, communicates module use instructions, and identifies the physical properties, and geometric orientation of the module within the vehicle's stack. Smart Systems - utilize the vehicle's systems to aid in assembly, checkout, launch, and transition to operational status. Autonomous Operations - broad spectrum of autonomy from; self-detect, isolation, and repair of anomalies to; self-guided, goal-following on-orbit activities. Minimally Structured Spacecraft - a spacecraft structural design that is driven by on-orbit activities, not launch load requirements. This SBIR Phase II program will develop the key enabling technologies required by a rapid response spacecraft architecture. The immediate benefits to the US military space community are two-fold. First, the technologies developed in this program can be quickly realized in flight hardware, as part of a Phase III program, and a near-term rapid response spacecraft demonstration conducted. Secondly, the developed technologies, in whole or in part, can be integrated into conventional spacecraft designs to improve their performance.

* information listed above is at the time of submission.

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