Development of ignition systems for 200N and 500N thrusters

First Page		Document Content
Date: 2010-04-20 04:01:17 Rocket engines Spacecraft propulsion Rocket propulsion Pyrotechnics Rocket propellants Liquid-propellant rocket Propellant RP-1 Ignition system Space technology Transport Rocketry		Development of ignition systems for 200N and 500N thrusters Add to Reading List Source URL: www.mai202.ru Download Document from Source Website File Size: 289,33 KB Share Document on Facebook

	PulCheR Pulsed Chemical Rocket with Green High Performance Propellants PulCheR 3rd WORKSHOP 5th CEAS Air & Space Conference DocID: 1g708 - View Document
	Test & Laboratory In our chemical laboratory dozens of composite and double base propellants for different applications have been developed specifically with characteristics like non-toxicity, minimum smoke, excellent ag DocID: 19GS1 - View Document
	GEL Propulsion In the last decades gel fuels and propellants have received increasing interest for applications in rocket and ramjet propulsion systems, because of their safety and performance benefits. Gelled propellant DocID: 19qzg - View Document
	SMART FUNCTIONAL NANOENERGETIC MATERIALS Richard A. Yetter Pennsylvania State University Multidisciplinary University Research Initiative (MURI) Program Review DocID: 19dA7 - View Document
	Moog – ISP Moog-ISP, formerly AMPAC In-Space Propulsion (ISP), is a leading developer and supplier of liquid rocket engines, tanks, and propulsion systems for commercial, defense, and spacecraft launch vehicles. Our DocID: 157rx - View Document