Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Tomoki Naya"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2012 (2012)
Ammonium-nitrate-(AN-) based composite propellants prepared with a hydroxyl-terminated polybutadiene (HTPB)/polytetrahydrofuran (PTHF) blend binder have unique thermal decomposition characteristics. In this study, the burning characteristics of AN/HT
Externí odkaz:
https://doaj.org/article/7fd683c3207344eaad2941e10ccb117a
Autor:
Makoto Kohga, Tomoki Naya
Publikováno v:
Journal of Energetic Materials. 33:288-304
Ammonium nitrate (AN)-based composite propellants have gained popularity because of the clean burning nature of AN as an oxidizer. However, such propellants have several disadvantages such as poor ignition and low burning rate. The burning characteri
Autor:
Tomoki Naya, Makoto Kohga
Publikováno v:
Journal of Propulsion and Power. 30:864-867
Autor:
Tomoki Naya, Makoto Kohga
Publikováno v:
Aerospace Science and Technology. 32:26-34
Research on the burning characteristics of propellants prepared with cyclotrimethylenetrinitramine (RDX) has not yet provided sufficient systematic experimental data. In this study, the thermal decomposition behaviors and the burning characteristics
Autor:
Tomoki Naya, Makoto Kohga
Publikováno v:
Aerospace Science and Technology. 27:209-215
Nitramine composite propellants have received significant attention in the field of solid rocket and gun propulsion. Cyclotetramethylene tetranitramine (HMX) is a nitramine compound that is well known as an energetic material. The burning characteris
Autor:
Makoto Kohga, Tomoki Naya
Publikováno v:
Propellants, Explosives, Pyrotechnics. 38:547-554
Autor:
Makoto Kohga, Tomoki Naya
Publikováno v:
Propellants, Explosives, Pyrotechnics. 38:87-94
Ammonium nitrate (AN)-based composite propellants have several major problems, namely, a low burning rate, poor ignitability, low energy, and high hygroscopicity. The addition of a burning catalyst proved to be effective in improving the burning char
Publikováno v:
Journal of Applied Polymer Science.
Polytetrahydrofuran (PTHF) is an effective binder ingredient used for improving the performance of propellants. PTHF becomes sufficiently rubbery for use as a binder with the addition of an adequate crosslinking modifier. This study investigated the
Publikováno v:
International Journal of Aerospace Engineering, Vol 2012 (2012)
Ammonium-nitrate-(AN-) based composite propellants prepared with a hydroxyl-terminated polybutadiene (HTPB)/polytetrahydrofuran (PTHF) blend binder have unique thermal decomposition characteristics. In this study, the burning characteristics of AN/HT
Publikováno v:
Medical Entomology and Zoology. 52:159