Laboratory Characterization of High Energy Materials
Abstract
AFN has demonstrated acceptable properties to further propellant development: displayed good stability (thermal, friction, impact and detonability), low melt point is suitable for monopropellant applications, and extremely low toxic vapor concentrations. AFN based propellant has been evaluated to indicate additional development is warranted: high performance demonstrated in thruster test bed, acceptable safety properties and low toxic vapor concentrations.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 10, 1999
- Accession Number
- ADA409421
Entities
People
- A. J. Brand
- I. M. Ismail
- M. B. Mckay
- T. W. Hawkins
Organizations
- Air Force Research Laboratory