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Hypersonic Control Modeling and Simulation Tool for Lifting Towed Ballutes, Phase I
Completed
Description
Global Aerospace Corporation proposes to develop a hypersonic control modeling and simulation tool for hypersonic aeroassist vehicles. Our control and simulation testbed will be focused on the particularly important problem of a lifting, towed ballute for planetary aerocapture. The importance of this technology innovation is in the understanding it can provide NASA on the control of hypersonic vehicles, in particular, of lifting towed ballutes. Lift control of a towed ballute will enable the use of smaller and lighter-weight ballutes for planetary orbit capture, which will make ballutes more attractive and feasible for missions to planets such as Neptune where high heating rates require extremely large ballutes for ballistic capture. The application of the comprehensive tool, to be developed in later phases, will be extensive including, but not limited to, control studies for entry and descent, aerocapture, and aero-gravity-assist with a range of hypersonic aeroassist systems (e.g. rigid and deployable aeroshells, waveriders, etc.). This proposal responds directly to the request in subtopic A2 to "leverage the foundational research to develop technologies and analytical tools focused on discipline-based solutions." In addition, in the hypersonic focus arena, we are responding directly to the interest in "system dynamic models incorporating the essential coupled dynamic elements with varying fidelity for control design, analysis and evaluation" and "simulation test beds for evaluating hypersonic concept vehicle control."
Details
| Technology area | Entry, Descent, and Landing > Aeroassist and Atmospheric Entry > Hypersonic Decelerators |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Langley Research Center, Hampton, VA |
| Start date | 2009-01-22 |
| End date | 2009-07-22 |
How to get involved
This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.
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