Multifunctional Aerogel Thermal Protection Systems for Hypersonic Vehicles

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,999.00
Award Year:
2008
Program:
SBIR
Phase:
Phase I
Contract:
NNX08CB27P
Award Id:
87977
Agency Tracking Number:
074618
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
30 Forbes Road, Northborough, MA, 01532
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
012924069
Principal Investigator:
Wendell Rhine
Principal Investigator
(508) 466-3130
wrhine@aerogel.com
Business Contact:
Heather Creelman
Business Official
(508) 691-1161
hcreelman@aerogel.com
Research Institution:
n/a
Abstract
The push to hypersonic flight regimes requires novel materials that are lightweight as well as thermally and structurally efficient for airframes and thermal protection systems to increase safety and decrease system weight. The materials required must maintain their performance throughout the lifetime of the system, without degrading over time or with use. A critical component of the system is the thermal protection system required to maintain internal temperatures compatible with the airframe. Currently available thermal protection system (TPS) designs and materials are not capable of providing the level of protection required by NASA without a significant increase in TPS weight and volume. In addition, current concepts for insulation utilize approaches that add nothing to the structural efficiency of the vehicle, or are made from materials that add unnecessary weight to achieve the required thermal performance. Therefore, NASA needs new TPS concepts for hypersonic vehicles that will provide the highest level of thermal performance and can also be structurally integrated with the airframe rather than just add parasitic weight. For this SBIR effort, Aspen proposes to develop a multifunctional aerogel that could be used in structurally integrated thermal protection systems to improve vehicle safety and decrease system weight.

* information listed above is at the time of submission.

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