Results 91 to 100 of about 4,253 (212)
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
Strategies for the production of maize-derived pharmaceuticals using cytoplasmic male sterile lines: In vitro tissue culture/transformation and field breeding approaches [PDF]
, 2009 Plant-made pharmaceuticals (PMPs) offer promise as efficient and cost-effective products for the treatment of human and animal diseases. An advantage of producing pharmaceuticals in maize is the large storage capacity and stability for proteins and ...
Frame, Bronwyn +4 more
core +2 more sources
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
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
Exploiting technological synergies for future launch vehicles [PDF]
, 2013 Two launch vehicle concepts based on technologies available today or in a short term future in Western Europe are presented. The design of both launchers has the goal of exploiting synergies with current European programs to limit development and ...
Burkhardt, Holger +5 more
core
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
Research on mechanical properties of HTPB propellants
Journal of Physics: Conference SeriesAbstract Slat propellants with different sizes and shapes are designed to investigate the strength criteria of HTPB propellants. According to the calculation and simulation results, with the increase of multiple, the designed size slat specimens can achieve equivalent biaxial tensile stress ratios of 1:2, 1:2.5, 1:3, 1:3.5, and 1:4 under
Chang Liu +4 more
openaire +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