SBIR-STTR Award

Development of Advanced Energetic Oxidizers for Solid Propellant applications.
Award last edited on: 11/6/2018

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$838,097
Award Phase
2
Solicitation Topic Code
N09-T017
Principal Investigator
Kurt Baum

Company Information

Fluorochem Inc

680 South Ayon Avenue
Azusa, CA 91702
   (626) 334-6714
   fluorochem@verizon.net
   www.fluorocheminc.com

Research Institution

University of Idaho

Phase I

Contract Number: N00014-09-M-0278
Start Date: 6/29/2009    Completed: 4/30/2010
Phase I year
2009
Phase I Amount
$99,949
The objective of this program is to design advanced energetic oxidizers superior to ammonium perchlorate (AP), develop methods for their preparation, and characterize the products.

Benefit:
The development of improved high energy oxidizers would provide the basis for advanced future generations of rocket propellants. These advances would benefit civilian as well as military applications, i.e., missile defense systems, tactical and strategic missiles, as well as commercial and military space access and strategic systems used in technologies associated with satellites.

Keywords:
chemical synthesis, chemical synthesis, Rocket propellants, nitro groups

Phase II

Contract Number: N00014-10-C-0456
Start Date: 9/16/2010    Completed: 6/16/2013
Phase II year
2010
Phase II Amount
$738,148
The objective of this program is to design advanced energetic oxidizers superior to ammonium perchlorate (AP), develop methods for their preparation, and characterize the products. The overall goal of the Phase II program with options is to make the technology ready for commercialization

Benefit:
The development of improved high energy oxidizers would provide the basis for advanced future generations of rocket propellants. These advances would benefit civilian as well as military applications, i.e., missile defense systems, tactical and strategic missiles, as well as commercial and military space access and strategic systems used in technologies associated with satellites.

Keywords:
chemical synthesis, Rocket propellants, nitro groups