SBIR/STTR Research Award
Investigation of Ignition Delay: Novel beta-Substituted Ethylazide Derivatives as Potential New Liquid Propellant Fuels
Award amount
$98,227Program and phase
SBIR · Phase IAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- AMERICAN PACIFIC CORP.
- Proposal award date
- 2005-05-27
- Contract end date
- 2006-03-01
- UEI
- VPQXQU2PUUB6
- Solicitation number
- 2005.1
- Topic code
- AF05-201
Research abstract
Few replacements for hydrazine-based propellants have been developed over the years. One potential candidate is 2-azido-N,N-dimethylethanamine (DMAZ). Unfortunately, DMAZ-IRFNA systems have exhibited ignition delays significantly longer than MMH-IRFNA systems. We are proposing the synthesis and testing of a novel â-substituted ethylazide derivatives that will overcome the longer ignition delays of DMAZ-IRFNA systems while maintaining or even enhancing performance. Thermochemical calculations show a comparable Isp between our novel â-substituted ethylazide derivatives and DMAZ or MMH, under equivalent operating conditions. Initial QSAR calculations indicate this material is significantly less toxic than hydrazine and its derivatives. These novel â-substituted ethylazide derivatives can be prepared in a simple two-step process from readily available starting materials. By leveraging our current R&D efforts and building upon collaborations already in place, we propose, in the Phase I effort, to synthesize quantities of this new material sufficient to obtain useful energetic and ignition delay data. This data will make a significant contribution to the search for new efficient fuels, with low environmental hazards for future propulsion systems.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Demonstration and Analysis of Reusable Launch Vehicle Operations
- Integrated Engine Health Management System
- Rocket Engine Health Management System - Turbopump System
- Demonstration and Analysis of Reusable Launch Vehicle Operations
- Integrated Vehicle Health Management "Intelligent Engine" Turbopump Concept