With the increasing of space activities and people’s awareness environmental protection, it is necessary to develop a new non-toxic propulsion system with high performance. Hydroxylammonium nitrate (HAN)/1-ethyl-3-methyl-imidazolium ethylsulfate([Emim][EtSO4]) blend ionic liquid propellant potential replacement high-performance characteristics for hydrazine type propellants, which can be used i...

Unguided reentry capsules are usually involved in ballistic entry. The final states (such as altitude and velocity of parachute activity) depend on initials parameters. Reentry trajectory parameters differently affect the thermal protection system (TPS), required deorbit propellant, and structural load. The purpose of this paper is to optimal design of deorbit parameters to minimize the thermal...

* Technical Program Manager † Visiting Scholar ‡ Research Scientist § Associate Professor of Civil and Environmental Engineering, University of Illinois at Urbana Copyright  2001 by Center for Simulation of Advanced Rockets. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Abstract We describe our numerical method for threedimensional simulations of s...

Recent experimentation has provided a more thorough understanding of the explosive response of class 1.3 composite propellant to severe impact. This study looked at an 88% total solids HTPB/Al/AP propellant similar to what could be used in space launch boosters. The program tested propellant charges as large as 22 inches in diameter. It includes hydrodynamic modeling for developing a basic unde...

A new planar structure of solid propellant micro -rocket for micro-spacecraft and Micro-Air-Vehicle applications is reported in this paper. We have successfully fabricated an array of micro-rockets using MEMS technology. For a lowpower consumption, the micro-igniter used here is a resistor deposited on a low tensile stress thin membrane to ensure a good heat transfer to the propellant. Experime...

The introduction of micro-spacecraft in the space industry has led to the development of various micro-propulsion techniques. Microthrusters are micropropulsion devices used in microspacecraft for precise station keeping, orbit adjustment, attitude control, drag compensation and apogee kicking. The principle of operation of a solid propellant thruster is based on the combustion of a solid energ...

In the paper short information about advantages of introduction detonation combustion to propulsion systems is briefly discussed and then research conducted at ?ukasiewicz-Institute Aviation on development rotating engines (RDE) presented. Special attention focused continuously (CRD), since it offers significant over pulsed (PD). Basic aspects initiation stability CRD are discussed. Examples ap...

The present study focuses simply on propellants which are environment friendly i.e. Green propellants. In Propulsion Systems, there are two ingredients burned together which are fuel & oxidizer and the resultant energy is used to propel the system. In composite solid rocket propellants, Ammonium perchlorate (AP) is being used extensively which has its own disadvantages i.e. HCl release during i...

The NASA Exploration Systems Architecture Study (ESAS) produced a transportation architecture for returning humans to the moon affordably and safely while using commercial services for tasks such as cargo delivery to low earth orbit (LEO). Another potential utilization of commercial services is the delivery of cryogenic propellants to LEO for use in lunar exploration activities. With in-space p...