Experimental and Advanced Nitrate-type Solid Propellants:
Investigating Slow-burning Compositions
(with the Rocket Science Institute)
This project aims to develop low-pressure, low-temperature exothermic formulations suitable for very small aeromodelling reaction motors, and other microjet applications. We’re developing modern versions of compositions similar to those originally developed for Jetex and Jet-X reloadable rocket motors. We intend to produce safe, non-explosive, "fuel pellets" that produces a large volume of non-toxic gases, and are safe for children to handle under adult supervision.
Guanidine nitrate and ammonium nitrate
are capable of self-sustained decomposition at very low pressures, and
with suitable catalysts have the potential for use indoors. Recent gas
generating patents suggest reactions that merit static test evaluation.
Current activities include on-line
research of chemicals and vendors, preparations for mixing and pellet production,
design of test motors and static test support equipment. Serious propellant
chemists, engineers, and technicians are welcome to inquire about participation.
Please send us a note with some information about your experience, related
education, and particular interests and abilities. People with good expertise
in small-scale machining, or thermochemistry, are especially invited to
collaborate with us. If you have experience with nitrate-type solid propellants,
by all means inquire.
The project is sponsored by the Rocket
Science Institute, Inc., and Microjet Propulsion Laboratory.