SBIR-STTR Award

High Performance Energetic Propellant Ingredient Process Research and Development
Award last edited on: 11/13/2018

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$150,000
Award Phase
1
Solicitation Topic Code
N16A-T021
Principal Investigator
Pascal Dube

Company Information

NALAS Engineering Services Inc

85 Westbrook Road
Centerbrook, CT 06409

Research Institution

University of Southern California

Phase I

Contract Number: N00014-16-P-1025
Start Date: 7/11/2016    Completed: 5/10/2017
Phase I year
2016
Phase I Amount
$150,000
Current state of the art oxidizers have been in service for decades, leaving the performance of our munitions and propulsion systems unchanged while our tactical objectives have increased in their requirements. Keeping with ongoing changes in the worlds military, maintaining a tactical advantage while meeting or exceeding mission capability requirements is of utmost importance for our nation. As such, the DoD thus requires a new generation of oxidizers with increased performance and reduced sensitivity to thermal, impact and shock stimuli. Specifically, these new oxidizers will have to show an energy greater than HMX while offering a sensitivity profile better than TNT. Moreover, an increase in impulse density and specific impulse (Isp) while offering a long service life is highly desirable especially if the material is also classified as insensitive. A key challenge is the development of novel compounds offering improved performance while maintaining suitable mechanical properties throughout the long service life. The identification, optimization and manufacture of the next generation of oxidizers requires a holistic approach to the problem. Our team will address this opportunity by enabling the rapid development of a new generation of energetic oxidizers for propellant formulations.

Benefit:
Demonstrate viability in an energetic formulation which permits a weapon system to meet mission capability requirements; exhibit sufficient mechanical and chemical robustness to meet service requirements over a wide temperature range to meet mission capability requirements

Keywords:
high-density, high-density, explosives, oxidizer, propellants, Scale-up, Propulsion

Phase II

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Start Date: 00/00/00    Completed: 00/00/00
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