Finite Element Multidisciplinary Simulation of a Reusable Launch Vehicle

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2003
Program:
STTR
Phase:
Phase I
Contract:
NAS4-03015
Award Id:
61684
Agency Tracking Number:
020037
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
4030 Lake Washington Blvd NE, 205, Kirkland, WA, 98033
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
PioFitzgerald
(425) 827-7476
pfitzgerald@stirling-dynamics.com
Business Contact:
PioFitzgerald
Business Official
(425) 827-7476
pfitzgerald@stirling-dynamics.com
Research Institute:
University of California Santa Barbara
Karen Hanson
UNIVERSITY OF CALIFORNIA
Santa Barbara, CA, 93106
(805) 893-3890
Nonprofit college or university
Abstract
Future research into advanced air vehicle designs will benefit from the continued improvement of analysis methods and software tools. A research program is proposed to provide enhanced capabilities to the NASA STARS software package in two key areas. These are; the addition of a control system toolbox including classical and modern control system design procedures, and the introduction of parallelization into the computational process. Since most current and planned high performance air vehicles depend heavily on their flight control systems, and their structure is designed for low weight, and an efficient propulsion system is essential, a fully integrated analysis is required in the design process to produce overall optimized performance. All these factors motivate the need for the newly proposed developments. Also, as more complexity is added to the analysis software, computer throughput productivity inevitably drops, despite computer advances, and this drives the need for parallelization. The capability resulting from this research promises significant increases in the scope and efficiency of STARS such that its use will have a greater range of application and will contribute to the assurance of safety in flight testing. The planned reusable launch vehicle will be the initial application objective of the enhanced software.

* information listed above is at the time of submission.

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