Results 211 to 220 of about 1,557,568 (278)

Biodegradability of Binder System Waste from Hydroxyl-Terminated Polybutadiene Propellant and Pretreatment for Biodegradation. [PDF]

Polymers (Basel)
Wu K, Chai T, Hu F, Ding Z, Wang C.
europepmc   +1 more source

Design, Fabrication, and Testing of a 3D-Printed Model Rocket with Integrated Telemetry Systems. [PDF]

Sensors (Basel)
Moschidis PG, Bithas PS, Meyer F.
europepmc   +1 more source

Preparation and Characterization of Porous Propellants by Template Leaching with PAAK. [PDF]

ACS Omega
Song Y, Zhou W, Xiao L, Jian X.
europepmc   +1 more source

Study on elongation master curve of thermal aging composite modified double base propellant. [PDF]

Sci Rep
Zheng J, Liu J, Deng H, Dang J, Yang C, Sun Z, Guo Z, Xu J, Chen X.   +8 more
europepmc   +1 more source

Novel glycidyl azide polymers containing aromatic diol units: synthesis and characterization for their application as energetic composite propellant binders. [PDF]

RSC Adv
Le-Nhat-Thuy G, Tuyet Anh DT, Hung VQ, Quynh Giang NT, Anh NT, Phuong HT, Thanh NH, Mai DT, Van Tuyen N.   +8 more
europepmc   +1 more source

Research on Time-Dimension Expansion of HBP Model Based on Hydroxyl-Terminated Polybutadiene (HTPB) Propellant Slurry. [PDF]

Polymers (Basel)
Bai Y, Wang J, Feng Y, Cao P, Jiang X.
europepmc   +1 more source

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INVESTIGATION OF SOLID PROPELLANT MICROTHRUSTERS

International Journal of Computational Engineering Science, 2003
A novel micropropulsion system is described for high-accuracy station keeping, attitude control and speed adjusting of microspacecraft. The proposed solid propellant microthruster is composed of two layers bonded together. One layer is a silicon layer, which contains a microchamber, a micronozzle and a 30-micron slot.
K. L. Zhang, S. K. Chou, Simon S. Ang, X. S. Tang, J. S. Phang   +4 more
openaire   +1 more source

Solid-propellant erosive burning

Journal of Propulsion and Power, 1987
A modeling approach based on experimental verification for the erosive burning of ammonium perchlorate composite propellants is proposed. It retains the idea that erosive burning is due to the penetration of the flow turbulence within the flame height and to the consequent enhancement of the transport coefficients and of the heat flux to the surface ...
J. GODON, J. DUTERQUE, G. LENGELLE
openaire   +1 more source

Detonability of Solid Composite Propellants

ARS Journal, 1961
The thin film pla t inum resistance thermometer (heat flux gage) has been successfully applied to measurement of heat fluxes from initiators for solid propellants. Hea t fluxes measured were as high as 1000 Btu/ft-sec from hot, particleladen reaction products of pyrotechnic igniters.
Andersen, W. H., Chaiken, R. F.
openaire   +2 more sources

Stability of Solid Propellant Combustion

Physical Review Letters, 1994
The stability of a combustion wave is one of the most important problems in combustion theory. The solution of the problem can be essentially simplified if the characteristic scales of the processes governing the combustion are small in comparison with the characteristic dimensions of the problem.
, Bychkov, , Liberman
openaire   +2 more sources