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Rotational Molding of Thermoplastic Cryogenic Propellant Tanks

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NAS8-02111
Agency Tracking Number: 013164
Amount: $596,943.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2002
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
2851 Commerce Street
Blacksburg, VA 24060
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Paul A. Clark,
 Principal Investigator
 (540) 953-4280
 clarkp@lunainnovations.com
Business Contact
 Garnett Linkous
Title: Chief Administrative Officer
Phone: (540) 953-4274
Email: linkousg@lunainnovations.com
Research Institution
N/A
Abstract

Rotational molding is a low-cost processing scheme used to fabricate large tanks, ducts, and tubes with complicated shapes. Rotational molding of liquid crystal polymer (LCP) resins was successfully demonstrated in the Phase I program, and the proposed Phase II effort will continue development of this process. LCP materials are of interest in application to cryogenic propellant storage because of their low permeability, low coefficient of thermal expansion (CTE), excellent strength, and chemical inertness. Development of rotationally molded LCP articles addresses the aerospace industry's need for lightweight, low-cost liners for use in propellant storage tanks and transport lines in space vehicles. LCP tanks will potentially be suitable for use with several liquid rocket propellant systems including liquid hydrogen, liquid oxygen, and hydrogen peroxide.

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

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