Search Results

High Performance HTPB-Based Energetic Nanomaterial with CuO Nanoparticles

Authors: de la Fuente, José Luis; Mosquera, Gonzalo; París, Rodrigo

Source: Journal of Nanoscience and Nanotechnology, Volume 9, Number 12, December 2009 , pp. 6851-6857(7)

Publisher: American Scientific Publishers

Preparation of CuO Modified SBA-15 and Applications as Catalyst in AP/HTPB Solid State Propellants

Authors: Tingming, Fu; Weifan, Chen; Zhiming, Gu; Lin, Liu; Fengsheng, Li

Source: Combustion Science and Technology, Volume 181, Number 6, June 2009 , pp. 892-901(10)

Publisher: Taylor and Francis Ltd

A neuro-optimal approach for thrust-insensitive trajectory planning

Authors: Pourtakdoust, S.H.; Pazooki, F.; Noushabadi, M. Fakhri

Source: Aircraft Engineering and Aerospace Technology: An International Journal, Volume 81, Number 3, 2009 , pp. 212-220(9)

Publisher: Emerald Group Publishing Limited

Effect of propellant morphology on acoustics in a planar rocket motor

Authors: Daimon, Y.; Jackson, T.; Topalian, V.; Freund, J.; Buckmaster, J.

Source: Theoretical and Computational Fluid Dynamics, Volume 23, Number 1, March 2009 , pp. 63-77(15)

Publisher: Springer

Simulation of axial combustion instability development and suppression in solid rocket motors

Author: Greatrix, David R.

Source: International Journal of Spray and Combustion Dynamics, Volume 1, Number 1, March 2009 , pp. 143-167(25)

Publisher: Multi-Science Publishing Co Ltd

Transient Combustion Response of AP/HTPB Composite Propellant to Acoustic Oscillations in a Rocket Motor

Authors: Cai, Weidong; Thakre, Piyush; Yang, Vigor

Source: Combustion Science and Technology, Volume 181, Number 4, April 2009 , pp. 597-617(21)

Publisher: Taylor and Francis Ltd

Infrared Emitted Intensity Measurements from Burning Aluminum Droplets in Solid Propellants

Authors: Harrison, J.; Brewster, Q.

Source: Combustion Science and Technology, Volume 181, Number 1, January 2009 , pp. 18-35(18)

Publisher: Taylor and Francis Ltd

Limitation of the ZN approach for calculating the response function of homogeneous propellants

Authors: Shusser, M.; Cohen, N.; Culick, F. E. C.

Source: Combustion Theory and Modelling, Volume 12, Number 6, December 2008 , pp. 1049-1054(6)

Publisher: Taylor and Francis Ltd

A Model of AP/HTPB Composite Propellant Combustion in Rocket-Motor Environments

Authors: Cai, Weidong; Thakre, Piyush; Yang, Vigor

Source: Combustion Science and Technology, Volume 180, Number 12, December 2008 , pp. 2143-2169(27)

Publisher: Taylor and Francis Ltd

Experimental evaluation and simulation on aging characteristics of aluminised AP-HTPB composite solid propellant

Authors: Kadiresh, P.N.; Sridhar, B.T.N.

Source: Materials Science and Technology, Volume 24, Number 4, April 2008 , pp. 406-412(7)

Publisher: Maney Publishing

Technology of Computational Fluid Dynamics in space engines and solar-gravity draught power plants

Author: Rugescu, Radu Dan

Source: International Journal of Energy Technology and Policy, Volume 6, Numbers 1-2, 4 February 2008 , pp. 124-142(19)

Publisher: Inderscience Publishers

A wireless addressing interface circuitry for microthruster array applications

Authors: Zhang, K.L.; Chou, S.K.; Ang, S.S.

Source: Aslib Proceedings: new information perspectives, Volume 79, Number 6, 2007 , pp. 628-634(7)

Publisher: Emerald Group Publishing Limited

Curvilinear deflagration of energetic materials

Authors: Kuznetsov, Igor R.; Stewart, D. Scott

Source: Combustion Theory and Modelling, Volume 11, Number 4, August 2007 , pp. 615-637(23)

Publisher: Taylor and Francis Ltd

Surface improvement of EPDM rubber by plasma treatment

Authors: Moraes, J.H.; A S da Silva Sobrinho,; Maciel, H.S.; Dutra, J.C.N.; Massi, M.; Mello, S.A.C.; Schreiner, W.H.

Source: Journal of Physics D: Applied Physics, Volume 40, Number 24, 21 December 2007 , pp. 7747-7752(6)

Publisher: Institute of Physics Publishing

Studies on a Novel Thermoplastic Polyurethane as a Binder for Extruded Composite Propellants

Authors: Mulage, K. S.; Patkar, R. N.; Deuskar, V. D.; Pundlik, S. M.; Kakade, S. D.; Gupta, M.

Source: Journal of Energetic Materials, Volume 25, Number 4, October 2007 , pp. 233-245(13)

Publisher: Taylor and Francis Ltd

A Modeling Investigation of Suppressant Distribution from a Prototype Solid-Propellant Gas-Generator Suppression System into a Simulated Aircraft Cargo Bay

Authors: Yoon, S. S.; Kim, H. Y.; Hewson, J. C.; Suo-Anttila, J. M.; Glaze, D. J.; DesJardin, P. E.

Source: Drying Technology, Volume 25, Number 6, June 2007 , pp. 1011-1023(13)

Publisher: Taylor and Francis Ltd

COMBUSTION OF A SOLID FUEL TUBE WITH CONTAINED LIQUID OXIDIZER IN A HOT GAS ATMOSPHERE

Source: Combustion Science and Technology, Volume 179, Numbers 1-2, January 2007 , pp. 265-280(16)

Publisher: Taylor and Francis Ltd

THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE

Source: Combustion Science and Technology, Volume 179, Numbers 5-6, May 2007 , pp. 1003-1027(25)

Publisher: Taylor and Francis Ltd

Adhesion in Solid Propellant Rocket Motors

Authors: Grythe, Kai Frode; Hansen, Finn Knut; Olsen, Torbjørn

Source: Journal of Adhesion, Volume 83, Number 3, March 2007 , pp. 223-254(32)

Publisher: Taylor and Francis Ltd

A wireless addressing interface circuitry for microthruster array applications

Authors: Zhang, K.L.; Chou, S.K.; Ang, S.S.

Source: Aircraft Engineering and Aerospace Technology: An International Journal, Volume 79, Number 6, 2007 , pp. 628-634(7)

Publisher: Emerald Group Publishing Limited