Results 71 to 80 of about 4,212 (194)
Transient processes in the combustion of nitramine propellants [PDF]
A transient combustion model of nitramine propellants is combined with an isentropic compression shock formation model to determine the role of nitramine propellant combustion in DDT, excluding effects associated with propellant structural properties or ...
Cohen, N. S., Strand, L. D.
core +1 more source
Reduced Reaction Mechanism for Rocket Nozzle Ablation Simulations [PDF]
, 2017 Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143107/1/6.2017-3682 ...
Boyd, Iain D., Cross, Peter G.
core +1 more source
Jurnal Teknologi Dirgantara, 2019 Pengembangan pengetahuan terhadap sifat rheologikal isian cair dari propelan berguna untuk mendapatkan sifat slurry yang optimum. Pengembangan ini dapat dimulai dari campuran HTPB-DOA sehingga penelitian ini bertujuan untuk mengetahui pengaruh DOA terhadap sifat rheologikal HTPB-DOA yang meliputi sifat alir terhadap shear rate, viskositas dan ...
Afni Restasari +3 more
openaire +1 more source
Catalytic effects of transition metal oxides on HTPB-based fuel polymer matrices
FirePhysChemLow regression rate due to difficult pyrolysis is a major challenge in the practical application of terminated hydroxyl‑terminated polybutadiene (HTPB)-based fuels in hybrid rocket propulsion.
Hongwei Gao +6 more
doaj +1 more source
Polímeros, 2004 O desenvolvimento de sistemas não-poluentes tem sido cada vez mais necessário para atender às exigências ambientais. Neste trabalho foram sintetizadas formulações de poliuretanos à base de água para a obtenção de membranas densas cujas propriedades ...
Fernanda M. B. Coutinho +2 more
doaj +1 more source
Solid Propulsion Integrity Program (SPIP) for verifiable enhanced solid rocket motor reliability [PDF]
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set common reliability goals for nozzles, cases, bondline, propellant, and insulation; (2) build a common engineering data base to support standard industry-wide ...
Butler, Barry L.
core +1 more source
Demonstration of a sterilizable solid rocket motor system [PDF]
A solid propellant rocket motor containing 60.9 Kg (134-lb) of propellant was successfully static fired after being subjected to eight heat sterilization cycles (three 54-hour cycles plus five 40-hour cycles) at 125 C (257 F).
Lambert, W. L. +2 more
core +1 more source
Ares V: A National Launch Asset for the 21st Century [PDF]
, 2009 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
Enhancement of the energetic performance of solid fuels with metal-fluoropolymer additives
FirePhysChemAluminum (Al) holds a pivotal role in augmenting the energetic potential of solid fuel formulations. Its incorporation can notably amplify the energy yield upon combustion.
Ayush Koul +6 more
doaj +1 more source
Technique for Evaluating the Erosive Properties of Ablative Internal Insulation Materials [PDF]
A technique for determining the average erosion rate versus Mach number of candidate internal insulation materials was developed for flight motor applications in 12 inch I.D. test firing hardware.
Hitner, J. M., McComb, J. C.
core +1 more source