Variable Specific Impulse Magnetoplasma Rocket - Document - PDFSEARCH.IO

First Page		Document Content
Date: 2009-07-29 16:07:44 Propulsion Variable Specific Impulse Magnetoplasma Rocket Ion thruster Plasma propulsion engine Fusion rocket Plasma Specific impulse Rocket engine nozzle Rocket engine Spacecraft propulsion Aerospace engineering Space technology		Add to Reading List Source URL: www.adastrarocket.com Download Document from Source Website File Size: 4,08 MB Share Document on Facebook

	Measuring thrust and predicting trajectory in model rocketry Michael Courtney and Amy Courtney Ballistics Testing Group, P.O. Box 24, West Point, NYAbstract: Methods are presented for DocID: 1pwlB - View Document
	COE CST Fifth Annual Technical Meeting Optical Measurements of Rocket Nozzle Thrust and Noise PI (s): Rajan Kumar & Farrukh Alvi DocID: 1p1q1 - View Document
	Measuring Nozzle Erosion with Ultrasound Pavan Narsai, Brian Cantwell Department of Aeronautics and Astronautics, Stanford University Introduction A major obstacle ahead of the use of long-burning hybrid rocket motors DocID: 11BtM - View Document
	CALIFORNIA STATE SCIENCE FAIR 2003 PROJECT SUMMARY Name(s) Christopher D. Edge DocID: Ak0F - View Document
	CALIFORNIA STATE SCIENCE FAIR 2003 PROJECT SUMMARY Name(s) Dylan E. James DocID: A6N9 - View Document