Results 41 to 50 of about 5,407 (249)
Study the Performance of Hydrazine Monopropellant Thruster Catalysts with Different Iridium Loading [PDF]
علوم، فناوری و کاربردهای فضایی, 2022 In this paper, the effects of different weight percentage of iridium (Ir) nanoparticles loadings on performance parameters of hydrazine catalyst and monopropellant thruster have been studied. Nanoparticles of iridium with different contents of 10 wt%, 20
Nooredin Ghadiri Massoom +5 more
doaj +1 more source
Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2019 In this paper, design and physical configuration of various components of a 10N Monopropellant Hydrazine Thruster focusing on design calculations and optimization of catalytic combustion chamber. According to this design, a prototype of the thruster will
Hadiseh Karimaei +3 more
doaj +1 more source
Effects of Geometrical Parameters of a Two-Sided Catalyst Bed on Flow and Thermal Fields of a Monopropellant Hydrazine Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2022 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
Foundations for Soft, Smart Matter by Active Mechanical Metamaterials
Advanced Science, Volume 7, Issue 18, September 23, 2020., 2020 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
Design and Simulation of Fuel Injector of a 10N Monopropellant Hydrazine Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2018 Monopropellant thruster of atitude control system is a requirement for the development and functionalization of satellites in space, which have expensive and high-tech technology.
Hadiseh Karimaei
doaj
Review of Scientific Instruments, 2021 A combustion assembly capable of continuously burning monopropellant and bipropellant liquid fuels at pressures up to 80 bars (1145 psig) was designed and constructed.
C. Fuller +5 more
semanticscholar +1 more source
Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite [PDF]
فصلنامه علوم و فناوری فضایی, 2011 This paper presents the multidisciplinary design optimization of monopropellant propulsion system of the nanosatellite for planner maneuver. Mass, configuration and internal ballistic equations are derived for any part of propulsion system (thruster ...
M. Nosratollahi, A. h. Adami-Dehkordi
doaj
AerospaceHydrogen peroxide is a promising oxidizer and monopropellant for space propulsion, offering a green alternative to conventional propellants. In combination with microencapsulated hydrocarbon fuels, a new type of monopropellant can be formed that unites ...
Robin Scholl +3 more
doaj +1 more source
Fast E-sail Uranus entry probe mission [PDF]
, 2014 The electric solar wind sail is a novel propellantless space propulsion concept. According to numerical estimates, the electric solar wind sail can produce a large total impulse per propulsion system mass.
Janhunen, Pekka +5 more
core +3 more sources
Design, test and build of a monopropellant thruster using 85% hydrogen peroxide
, 2021 The objective of this research is to design, build, and test about a 5N Hydrogen Peroxide(H2O2) monopropellant thruster (MPT). It is utilized in remote sensing satellites for attitude control and orbit manoeuvres. The MPT uses high test peroxide (HTP) of
A. Deif +3 more
semanticscholar +1 more source