Results 111 to 120 of about 1,895 (230)
Ammonium perchlorate (AP) has been the oxidizer of choice for composite solid propellants for decades and has been the object of decomposition studies for safety monitoring.
Andrew R. Demko +4 more
doaj +1 more source
Use of Taguchi design of experiments to optimize and increase robustness of preliminary designs [PDF]
The research performed this summer includes the completion of work begun last summer in support of the Air Launched Personnel Launch System parametric study, providing support on the development of the test matrices for the plume experiments in the Plume
Carrasco, Hector R.
core +1 more source
Mechanical properties of HTPB propellants: Recent advances and underlying mechanisms
Hydroxyl-terminated polybutadiene (HTPB)-based composite solid propellants (CSPs) are widely used in solid rocket motors due to their excellent mechanical properties and low cost.
Wasiullah Qazi +3 more
doaj +1 more source
Curing Properties of HTPB-based Solid Propellants
Su-A Jeon +4 more
openaire +1 more source
A feasibility study for Scout polar launches from NASA Wallops Flight Center [PDF]
The feasibility of launching the Scout vehicle into a polar orbit from Wallops Flight Center is discussed. The impact of proposed flights on vehicle hardware and range safety are defined.
Myler, T. R.
core +1 more source
Ares V: A National Launch Asset for the 21st Century [PDF]
NASA is designing the Ares V as the cargo launch vehicle to carry NASA's exploration plans into the 21st century. The Ares V is the heavy-lift component of NASA's dual-launch architecture that will replace the current space shuttle fleet, complete the ...
Creech, Steve, Sumrall, Phil
core +1 more source
An in-depth understanding of the behaviours of solid propellants under low-velocity impact loads is crucial for enhancing their safety in applications such as aerospace propulsion.
Yiming Zhang +6 more
doaj +1 more source
Hybrid Propulsion Technology Program [PDF]
Future launch systems of the United States will require improvements in booster safety, reliability, and cost. In order to increase payload capabilities, performance improvements are also desirable.
Holzman, A. L., Jensen, G. E.
core +1 more source
Catalyst Screening for Ammonium Nitrate Oxidizer [PDF]
Arosio, L., Galfetti, L., Maggi, F.
core +1 more source
Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders [PDF]
Cristilli, F. +6 more
core +1 more source

