About this document
Ad 0769283 by harrypotter082003 is a document available to read on EtoBox.
The document evaluates the feasibility of the powder rocket concept through a series of combustor tests using ammonium perchlorate/aluminum propellants at various thrust levels. Key findings indicate that particle size significantly affects combustion stability, with optimal performance observed at specific particle sizes, although issues such as injector plugging were noted. The study also includes laboratory investigations on powder packing to maximize density, yielding important insights on performance e
- Author
- harrypotter082003
- Language
- EN