Results 121 to 130 of about 17,155 (237)

The bond stress in a viscoelastic propellant disk during thermal shock [PDF]

Analysis of bond stress in viscoelastic case bonded solid propellant rocket assembly during thermal ...
Levitsky, M., Shaffer, B. W.
core   +1 more source

Studies of nozzle ablative material performance for large solid boosters Final report [PDF]

Carbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket ...
Dahm, T. J., Schaefer, J. W.
core   +1 more source

Flexible Three-Dimensional Stress Sensor for Embedded Monitoring of Solid Rocket Propellant. [PDF]

Micromachines (Basel)
Shi Y, Lü X, Ren K, Zhu W.
europepmc   +1 more source

First applications of ultrasound technology in solid rocket propellant combustion promotion. [PDF]

Ultrason Sonochem
Wen Z, Jing H, Hao F, Wang Y, Kuang B, Liu P, Ao W.   +6 more
europepmc   +1 more source

Solid rocket motor internal insulation [PDF]

Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant.
Keller, R. B., Jr., Twichell, S. E.
core   +1 more source

Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]

Polymers (Basel)
Chmielarek M, Szczęśniak B, Blacharski K.   +2 more
europepmc   +1 more source

Theoretical study of the ballistics and heat transfer in spinning solid propellant rocket motors [PDF]

Computerized prediction analyses of radial spin acceleration effects on solid propellant rocket motor ballistics and heat ...
Hodge, B. K., Whitesides, R. H., Jr.
core   +1 more source

Three-dimensional finite element analysis of acoustic instability of solid propellant rocket motors [PDF]

A three dimensional finite element solution of the acoustic vibration problem in a solid propellant rocket motor is presented. The solution yields the natural circular frequencies of vibration and the corresponding acoustic pressure mode shapes ...
Hackett, R. M., Juruf, R. S.
core   +1 more source

Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]

Polymers (Basel)
Feng F, Chen X, Xu J, Zeng Y, Huang W, Dong J.   +5 more
europepmc   +1 more source

Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus. [PDF]

Sci Rep
Yao L, Jinsheng X, Changsheng Z, Xiong C, Xiumin Y.   +4 more
europepmc   +1 more source