Results 151 to 160 of about 370 (179)
Some of the next articles are maybe not open access.

Structure‐property relationship of HTPB‐based propellants. I. Effect of hydroxyl value of HTPB resin

Journal of Applied Polymer Science, 1993
AbstractComposite propellants based on hydroxyl‐terminated polybutadience (HTPB) resin are the most common contemporary solid propellants for launch vehicle and missile applications. A series of HTPB resins, manufactured by free‐radical polymerisation using a peroxide initiator, with varying molecular weights and hydroxyl values, was used in propellant
R. Manjari   +3 more
openaire   +1 more source

Aging of HTPB Propellant

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005
Moshe Kivity   +2 more
openaire   +1 more source

Aging Characteristics of HTPB Propellant Based on Volume Resistivity

Propellants, Explosives, Pyrotechnics
ABSTRACTHydroxyl‐terminated polybutadiene (HTPB) propellant faces the problem of aging from casting to use. Generally, the aging degree of HTPB propellant is evaluated by a destructive mechanical property test. Therefore, it is necessary to seek a new evaluation method. Electrical performance is a method that can achieve nondestructive testing. However,
Lina Xie   +10 more
openaire   +1 more source

HTPB propellant aging and service life

16th Joint Propulsion Conference, 1980
A. CHRISTIANSEN, L. LAYTON, R. CARPENTER
openaire   +1 more source

Development of HTPB propellants for the SRAM motor

16th Aerospace Sciences Meeting, 1978
L. MCGEE   +3 more
openaire   +1 more source

Development of HTPB binder for solid propellant

24th Joint Propulsion Conference, 1988
KATSUAKI KOSAKA   +4 more
openaire   +1 more source

Molecular Dynamics Study on Aging Mechanism of HTPB Propellants

Springer Proceedings in Physics, 2022
Liping Jiang   +2 more
exaly  

Home - About - Disclaimer - Privacy