Results 151 to 160 of about 1,875 (170)

Development and Test of a Miniature Hydrogen Peroxide Monopropellant Thruster

42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006
Analysis of present and future missions concluded that a miniaturised hydrogen peroxide monopropellant rocket engine is the optimum solution for the increasing demand for small and low cost propulsion systems for small satellites. The attractiveness of monopropellant thrusters is based on its operational and structural simplicity.
Carsten Scharlemann, M. Schiebl, K. Marhold, Martin Tajmar, P. Miotti, C. Kappenstein, Y. Batonneau, R Brahmi, C. Hunter   +8 more
openaire   +1 more source

Model for N₂O monopropellant thruster operation

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2008
The current paper presents a new model for the simulation of a prospective nitrous oxide (N2O) monopropellant thruster operation. The specific impulse performance expected by the N2O monopropellant is suitable for spacecraft station-keeping and small orbit manoeuvres.
V Zakirov, H Zhang
openaire   +1 more source

A monopropellant hydrazine MEMS thruster for attitude control of nanosatellites

2010 IEEE Students Technology Symposium (TechSym), 2010
This paper highlights the design and development of catalytic type mono-propellant hydrazine microthruster for space applications. In the process of development of microthruster the modeling & simulation of different parts/modules have been considered. Design of inlet feed channel and exit nozzle with different layout have been done to achieve required
null Pijus Kundu, T. K. Bhattacharyya, S. Das   +2 more
openaire   +1 more source

Monopropellant-Electrospray Multimode Thruster Testing Results: Electrospray Mode

AIAA Propulsion and Energy 2021 Forum, 2021
Christopher T. Lyne, Joshua Rovey, Steven P. Berg   +2 more
openaire   +1 more source

Modeling of MEMS-Based Hydrogen Peroxide Monopropellant Micro-Thrusters

2006
Abstract : This document describes the three-year effort to develop computational methodologies for the modeling of a hydrogen-peroxide based monopropellant micro-thruster operation. Computational models have been developed in two primary areas: (1) the numerical simulation of supersonic viscous flow in linear micronozzles; and (2) numerical simulation
openaire   +1 more source

Green Ionic Liquid Multimode Monopropellant Based Chemical Micro-thruster

AIAA SCITECH 2022 Forum, 2022
Animesh Sharma, Anthony C. Adducci, Joshua Rovey, Chengyu Ma, Charles N. Ryan, Steven Berg, Michael Lembeck, Zachary R. Putnam   +7 more
openaire   +1 more source

Pressure Oscillation Amplification of Pulse Modulated Monopropellant Thruster

2018 Joint Propulsion Conference, 2018
Sukmin Choi, Kijeong Yu, Sejin Kwon
openaire   +1 more source

A survey of monopropellant hydrazine thruster technology

9th Propulsion Conference, 1973
openaire   +1 more source

EXPERIMENTAL ASSESSMENT OF HYDROGEN PEROXIDE DECOMPOSITION IN A MONOPROPELLANT THRUSTER

International Journal of Energetic Materials and Chemical Propulsion, 2011
BONIFACIO, SALVATORE, FESTA, GIANDOMENICO, RUSSO, ANNAMARIA   +2 more
openaire   +2 more sources

Monopropellant Hydrazine Thrusters—Bringing Updated Designs to Flight

52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Vincent Yarnot, Matthew B. Dawson, Olwen M. Morgan   +2 more
openaire   +1 more source