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Low Mass Aeroshell Deployment Mechanism

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNM07AA47C
Agency Tracking Number: 065939
Amount: $99,993.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: S7.04
Solicitation Number: N/A
Timeline
Solicitation Year: 2006
Award Year: 2007
Award Start Date (Proposal Award Date): 2007-01-19
Award End Date (Contract End Date): 2007-07-23
Small Business Information
2750 Indian Ripple Rd.
Dayton, OH 45440-3638
United States
DUNS: 130020209
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Stephen Vining
 Principal Investigator
 (937) 320-1877
 viningsd@crgrp.net
Business Contact
 Patrick Hood
Title: Business Official
Phone: (937) 320-1877
Email: hoodpj@crgrp.net
Research Institution
N/A
Abstract

Cornerstone Research Group Inc. (CRG) will develop new shape memory polymer (SMP) deployment mechanisms for actuating thermal protective systems (TPS) panels to create a deployable large surface area aeroshell. This innovation will utilize VeriflexTM -- CRG's high performance SMP material -- to create a low mass actuation system for a deployable the aeroshell design. VeriflexTM-based mechanisms will deploy the aeroshell without the use of motors, springs, or mechanical controls. These simple, self-deploying, self-aligning mechanisms will reduce the mass and the complexity of the aeroshell design. VeriflexTM-based deployment mechanisms will allow the use of panels made from existing TPS materials to create a large surface area aeroshells that will stow in a highly compact pre-launch and storage configuration and then self-deploy before reentry to the operational configuration. The TPS panels will deploy outward and increase the diameter of the aeroshell. For every 10 percent increase in the diameter, there will be a 21 percent increase in the total surface area of the aeroshell. The relative volume of space needed to stow the reentry vehicle would not increase.

* Information listed above is at the time of submission. *

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