SBIR/STTR Research Award
System for Aero, Servo, Thermal, Elastic, Propulsion (ASTEP) Coupled Analysis
Award amount
$99,997Program and phase
STTR · Phase IAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- M4 ENGINEERING, INC.
- Proposal award date
- 2005-08-05
- Contract end date
- 2006-05-05
- UEI
- DM3EW67JLQM1
- Solicitation number
- Not reported
- Topic code
- AF05-T027
Research abstract
We will implement a high fidelity multidisciplinary analysis process for coupled aero-servo-thermo-elastic-propulsion analysis of hypersonic waveriders. Our approach allows the use of Navier-Stokes CFD coupled with ablation, propulsion, and finite element models, but in a novel way that allows efficient analysis of entire flight trajectories.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Hypersonic Computational Fluid Dynamics Heat Flux Sub-Models
- PyFoil81: Rotorcraft Design Tool Airfoil Table Generator
- High-Fidelity Computational Modeling of Fluid-Thermal-Structural Interactions in Hypersonic Air-Breathing Systems
- UAM Design Space Exploration Framework with Embedded Version Control
- Low Cost Carbon-Carbon Development for Hypersonic Flight Systems
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Integrated Aero-Servo-Thermo-Populso-Elasticity (ASTPE) for Hypersonic Scramjet Vehicle Design/Analysis
- Integrated Aero-Servo-Thermo-Populso-Elasticity (ASTPE) for Hypersonic Scramjet Vehicle Design/Analysis
- Aeroservothermoelastic Modeling for a Hypersonic Wave Rider Vehicle
Research funding history
83 SBIR/STTR records share this UEI (2004–2026). Reported award amounts total $30,097,301. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration