Results 31 to 40 of about 5,407 (249)
Existing autonomous pneumatic soft robots have a stiff fuel tank to transport the fuel and inflate the actuator. Inspired by pit membranes in trees, a chemical pump decouples the pressures of the fuel tank and actuator, while the fuel is transmitted to the actuator against the pressure difference.
Junsoo Kim, Kai Luo, Zhigang Suo
wiley +1 more source
The present research investigates a case study on thermal design and improvement of hydrazine monopropellant pipelines based on actual cases, in order to highlight the critical factors for thermal design when developing an onboard propulsion system for a
Kyun Ho Lee +3 more
doaj +1 more source
Design and Analysis of Pressure- Swirl Fuel Injector with Full- Cone Spray for Catalytic Thruster [PDF]
The monopropellant thrusters of the situation control system are a requirement for the development and application of satellites and space capsules in space, which are high-tech and expensive. In this paper, the design and simulation of a pressure- swirl
Hadiseh Karimaei
doaj +1 more source
Aluminized Enhanced Blast Explosive Based on Polysiloxane Binder
Abstract Drastic measures are taken in order to improve the properties of enhanced blast explosives. First, a binder with high reactivity as reducing agent is selected. The binder, platinum cure silicone, generates pyrophoric decomposition products in situ during the detonation.
Stefan K. Kolev, Tsvetomir T. Tsonev
wiley +1 more source
Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse. However, its ignition and combustion process are complex and need to be better understood.
Chengyin Tu +8 more
wiley +1 more source
Abstract For a class of conic‐type non‐linear time‐delay Markov jump systems, the asynchronous dissipative output feedback controller based on the guaranteed cost control and quantiser is designed in this study. In real applications, the system and the controller modes are always non‐synchronous, so we introduce the hidden Markov model to solve this ...
Xiang Zhang +3 more
wiley +1 more source
FMECA-Based Risk Assessment in Monopropellant Hydrazine Propulsion System [PDF]
The Monopropellant Hydrazine Propulsion system is one of the most widely used types of single-agent propulsion systems to control the position or correction of satellites in orbits.
Mohammad Nadjafi +2 more
doaj +1 more source
Optimization of 10 N Monopropellant High Test Peroxide Thruster for Space Applications
Monopropellant thruster is one of the most propulsion system types developed in the space industry. This system uses a single type of propellant that reacts in porous medium catalytic packed bed to generate thrust in the form of hot gases.
Fadela Benzenine +3 more
semanticscholar +1 more source
Geometrical characterization and performance optimization of monopropellant thruster injector
The function of the injector in a monopropellant thruster is to atomize the liquid hydrazine and to distribute it over the catalyst bed as uniformly as possible. A second objective is to place the maximum amount of catalyst in contact with the propellant
T.R. Nada, A.A. Hashem
doaj +1 more source
Multidisciplinary Design Sensitivity Analysis of a Spacecraft Monopropellant Propulsion system by Latin Hypercube Sampling (LHS) [PDF]
Accurate solving of complex systems such as spacecraft is very costly and time consuming. By building a surrogate model, the solution time and the cost can be reduced.
Mohammad Hossein mansouri Moghari +2 more
doaj +1 more source

