Results 91 to 100 of about 449 (191)

Performance of composite solid rocket propellants for rocket assisted projectiles (RAP) [PDF]

The International Conference on Chemical and Environmental Engineering, 2016
Mohamed Nawwar, Tamer Wafy, Hossam Mustafa   +2 more
openaire   +1 more source

The Rise and Fall of the Hiram–Solomon Alliance: Zionist, Hebrew and Lebanese Nationalism, and the 1982 Israeli Invasion of Lebanon

Nations and Nationalism, EarlyView.
Asher Kaufman
wiley   +1 more source

NUMERICAL STUDIES ON FLOW BEHAVIOR OF COMPOSITE PROPELLANT SLURRY DURING VACUUM CASTING DOI 10.5028/jatm.2012.04021212

Journal of Aerospace Technology and Management, 2012
Rockets are powered by composite solid propellant, which is a heterogeneous system consisting of solid oxidizer and metallic fuel dispersed in a polymeric fuel binder matrix.
Praveen Prakash Singh, Bikash Bhattacharya, Bejoy Thiyyarkandy, Mukesh Jain, Ganesh Shankar Dombe, Mehilal Mehilal   +5 more
doaj  

Blistering barnacles: Space physiology in The Adventures of Tintin

Experimental Physiology, EarlyView.
Jacob P. Hartmann, Mathis B. Mottelson, Rasmus H. Dahl, Ronni R. Plovsing, Ronan M. G. Berg   +4 more
wiley   +1 more source

Anomalous Behavior of a Solid Rocket Motor Nozzle Insert During Static Firing Test

Journal of Aerospace Technology and Management, 2016
This paper presents the study and development of a firing test used to evaluate the behavior of a solid rocket motor. The motivation for the development of a subscale solid rocket motor with end burning propellant grain geometry arose from the need to ...
Ronald Izidoro Reis, Wilson Kiyoshi Shimote, Luiz Cláudio Pardini   +2 more
doaj  

A Reliable Method for Predicting the Specific Impulse of Chemical Propellants

Journal of Aerospace Technology and Management, 2018
The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
doaj  

Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies

Applied Sciences
Challenges in the traditional cast-and-cure manufacturing of composite solid propellants, such as the use of mandrels and the toxicity of curing agents, are being addressed through new propellant formulations and additive manufacturing techniques. Within
Filippo Masseni, Giacomo Tetti, Alessandra Zumbo, Camilla Noé, Giovanni Polizzi, Leonardo Stumpo, Andrea Ferrero, Dario Pastrone   +7 more
doaj   +1 more source

Experimental study on the porosity of HTPB propellant: characterization of damage evolution

Journal of Materials Research and Technology
To characterize the damage evolution mechanism of HTPB composite solid propellant, the porosity as well as the sphericity will be analyzed using micro-CT. Under normal temperature and pressure, the damage mechanisms include voids, ''dewetting'' damage at
Huihui Zhang, Ruyan Zhao, Zhibin Shen, Haiyang Li, Dapeng Zhang, Kuangwei Deng   +5 more
doaj   +1 more source

Chemically Collapsible Mandrel for Solid Rocket Motor Processing

Journal of Aerospace Technology and Management, 2015
Composite propellant mainly consists of two parts, binder matrix (prepolymer, plasticizer, cross linker, antioxidant and curative etc.) and solid ingredients (oxidizer, metal fuel, burn rate modifier, combustion stabilizer etc.).
Abhijit Dey, Arvind Kumar, Arun K Sikder, Manoj Gupta   +3 more
doaj  

Improving the Mechanical Properties of Composite Rocket Propellants

, 2004
Solid composite rocket propellants usually contain ammoniumperchlorate embedded in an elastic polymer binder. The bindercan be based on a liquid prepolymer such as hydroxyl-terminatedpolybutadiene, HTPB, or poly(3-nitratomethyl-3-methyl oxetane,PolyNIMMO.
openaire   +1 more source