Abstract: The invention relates to propellant compositions comprising a solid inorganic perchlorate oxidizing agent, a nitrogen-containing fuel, and a burn rate catalyst. Such compositions may be used as a propellant material, (e.g., in rocketry), a pyrotechnic material, an explosive material, a light generating material, a heat generating material, or a sound generating material.
Abstract: Methods and systems for controlling model aircraft are provided. In one aspect, a model aircraft includes a section having a longitudinal axis that extends from a rear of the aircraft to a front of the aircraft, the longitudinal axis being substantially parallel to a surface of the Earth when the aircraft is in level flight, and the aircraft includes a control system.
Abstract: The invention relates to propellant compositions comprising a solid inorganic perchlorate oxidizing agent, a nitrogen-containing fuel, and a burn rate catalyst. Such compositions may be used as a propellant material, (e.g., in rocketry), a pyrotechnic material, an explosive material, a light generating material, a heat generating material, or a sound generating material.
Type:
Application
Filed:
November 14, 2002
Publication date:
May 20, 2004
Applicant:
Estes-Cox Corporation
Inventors:
Scott James Dixon, Barry Richard Tunick, Edwin Duane Brown