Effects of Geometrical Parameters of a Two-Sided Catalyst Bed on Flow and Thermal Fields of a Monopropellant Hydrazine Thruster [PDF]
In present study, a hydrazine based monopropellant thruster decomposition chamber is simulated numerically. The catalyst bed separated in two sides, the particles size in upstream side is larger than those in downstream side.
Mohammad Reza Salimi
doaj +1 more source
Combustion Wave Structure of the Ammonium Dinitramide‐Based Ionic Liquid Propellant
Abstract The ammonium dinitramide‐based ionic liquid propellant (ADN‐based ILP), which is a mixture of ADN, monomethylamine nitrate (MMAN), and urea, is a low toxic monopropellant with a higher performance than that of hydrazine. To clarify the combustion wave structure of ADN‐based ILP, which has low volatility, we focused on the relationship between ...
Yuichiro Ide +5 more
wiley +1 more source
Microfluidic Tissue Engineering and Bio‐Actuation
Microfluidics enables the engineering of biological tissues through micro‐precision control over the cell microenvironment, fabrication of cell‐laden matrices, and distribution of fluids to perfuse 3D tissue constructs. In particular, microfluidically‐advanced functional muscle tissues can be used as performant actuators in the next generation of bio ...
Miriam Filippi +4 more
wiley +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
Effect of Injector Pressure Drop on The Performance of A 1 N Monopropellant Thruster [PDF]
The effects of injector pressure drop on the performance of a catalytic reactor are studied experimentally. The injectors were simple orifices. Dynamic interactions between the injector and the reactor determine the transient behavior of the system ...
Alireza Rajabi +6 more
doaj +1 more source
Low Cost Catalysts for Hydrazine Monopropellant Thrusters [PDF]
Hydrazine monopropellant engines are widely used in space missions; mainly in reaction control systems. The most widely used catalyst is the aluminum oxide supported iridium. It is also very expensive. The cost of the catalyst weights heavily, especially in the high thrust, short life thrusters used for roll control of launch vehicles. In this paper we
José Hinckel +4 more
openaire +1 more source
Micro Coriolis mass flow censor with extended range for a monopropellant micro propulsion system [PDF]
We have designed and realised a micromachined micro Coriolis flow sensor for the measurement of hydrazine (N2H4, High Purity Grade) propellant flow in micro chemical propulsion systems.
Dijkstra, M.A. +5 more
core +10 more sources
Reactor Structure for the Decomposition of ADN-Based Monopropellant
Ammonia dinitramide (ADN)-based liquid monopropellants are considered to be environmentally friendly alternatives to the toxic and carcinogenic hydrazine-based propellants. Hence, Space Solutions Co., Ltd.
Wonjae Yoon +2 more
doaj +1 more source
Effect of Spherical Silver Particles Size of the Catalyst Bed on Hydrogen Peroxide Monopropellant Thruster Performance [PDF]
In this paper, an analytical approach combined with a two-dimensional computational fluid dynamics (CFD) model is pursued to simulate the fluid flow in a monopropellant thruster for satellite propulsion systems.
F. Benzenine +3 more
doaj +1 more source
Foundations for Soft, Smart Matter by Active Mechanical Metamaterials
An emerging field of active mechanical metamaterials establishes foundations for soft, smart engineered matter that may autonomously operate in diverse future applications. This Review surveys advances in mechanical design, material formulation, sensory mechanisms, and control integration that are strategically synthesized in active mechanical ...
Maya Pishvar, Ryan L. Harne
wiley +1 more source

