Self-healing Nanocomposites for Reusable Composite Cryotanks

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$124,997.00
Award Year:
2012
Program:
SBIR
Phase:
Phase I
Contract:
NNX12CF42P
Award Id:
n/a
Agency Tracking Number:
115206
Solicitation Year:
2011
Solicitation Topic Code:
O2.04
Solicitation Number:
n/a
Small Business Information
NJ, Piscataway, NJ, 08854-3723
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
042939277
Principal Investigator:
DanielEberly
Principal Investigator
(732) 868-3141
deberly@neicorporation.com
Business Contact:
GaneshSkandan
CEO
(732) 868-3141
gskandan@neicorporation.com
Research Institute:
Stub




Abstract
Composite cryotanks, or Composite Overwrapped Pressure Vessels (COPVs), offer advantages over currently used aluminum-lithium cryotanks, particularly with respect to weight savings. Future NASA missions are expected to use COPVs in spaceflight propellant tanks to store fuels, oxidizers, and other liquids for launch and space exploration vehicles. However, reliability and reusability of the COPVs are of concern, especially in cryogenic temperature applications; this limits adoption of COPVs in future reusable vehicle designs. The major problem with composites is the inherent brittleness of the epoxy matrix, which is prone to microcrack formation, either from exposure to cryogenic conditions or from impact from different sources. If not prevented, the microcracks can grow into larger cracks, leading to catastrophic failure and loss of function of the composite. In addition, the presence of microcracks increases gas permeation and leakage, which is undesirable in a COPV. Accordingly, materials innovations are needed to mitigate microcrack formation in composite cryotanks. In Phase I we propose to demonstrate microcrack prevention and mitigation in COPVs through the use of a novel nanocomposite matrix containing engineered nanoscale materials which will also enable self-healing of microcracks. Phase II will build upon the Phase I program to enable a TRL 5-6 working proof of concept and prototype for NASA testing, capable of long term use with high cycle performance at cryogenic temperatures.

* information listed above is at the time of submission.

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