Summary of results of ground testing of spinning solid rockets, with particular emphasis on motors used as sounding rockets, and comparison of data to free-flight results; motors discussed include Bristol Aerospace, Black Brant III; Aerojet General Corp, ALCOR IA; Thiokoi Chemical Corp, TE-388; Lockheed Propulsion Co, HYDAC I and II; and Naval Ordnance Test Station NOTS 551; principle effects noted have been associated with accelerations to fundamental propellant combustion and flow processes, and deposition of hot combustion residue within motor chamber.
Spin acceleration effects on some full-scale rocket motors
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 5 , n 2
1968
5 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Acceleration effects in solid propellant rocket motors
TIBKAT | 1985
|Acceleration effects in solid propellant rocket motors
AIAA | 1986
|