<--- Back to Details
First PageDocument Content
Spacecraft propulsion / Reusable launch system / Liquid air cycle engine / Single-stage-to-orbit / Falcon / Two-stage-to-orbit / N1 / Spaceplane / Sputnik / Aerospace engineering / Space technology / Spaceflight
Date: 2015-03-09 22:49:05
Spacecraft propulsion
Reusable launch system
Liquid air cycle engine
Single-stage-to-orbit
Falcon
Two-stage-to-orbit
N1
Spaceplane
Sputnik
Aerospace engineering
Space technology
Spaceflight

Microsoft Word - RIspace_Paper_28(DSalt)_v6.doc

Add to Reading List

Source URL: www.space-access.org

Download Document from Source Website

File Size: 1,25 MB

Share Document on Facebook

Similar Documents

Jet engines / Internal combustion engine / Spaceflight / Spacecraft propulsion / Propulsion / Single-stage-to-orbit / Fluid dynamics / Aircraft engines / Scramjet / Combustor / Ramjet / Particle image velocimetry

Microsoft Word - VSGC_conf13_paper_draft5

DocID: 1rqqS - View Document

Aircraft engines / Jet engines / Single-stage-to-orbit / Spacecraft propulsion / Spaceflight / Business / Space access / University of Virginia / Scramjet / Uva / Economy

StudentConf agenda-2011-Final.xlsx

DocID: 1pVq8 - View Document

Aircraft engines / Jet engines / Single-stage-to-orbit / Space access / Spacecraft propulsion / Business / Spaceflight / Propulsion / University of Virginia / University of Amsterdam / Lidar / Uva

Virginia Space Grant Consortium Student Research Conference Agenda Hampton University Student Center, Hampton, Va. April 9, 2009 8:00-8:30

DocID: 1pREH - View Document

Jet engines / Fluid dynamics / Spacecraft propulsion / Single-stage-to-orbit / Measurement / Scramjet / Combustor / Hy-V / Ramjet / Flow measurement / Particle image velocimetry / Shock wave

Characterization of a Dual-Mode Scramjet Combustor via Stereoscopic Particle Image Velocimetry Author: Brian Rice Advisor: Chris Goyne and Jim McDaniel University of Virginia Abstract

DocID: 1pDxn - View Document

Jet engines / Fluid dynamics / Measurement / Single-stage-to-orbit / Aircraft engines / Scramjet / Wind tunnel / Indium tin oxide / Particle image velocimetry / Velocimetry / Combustor / Ramjet

REDUCTION OF TRIBOELECTRIC CHARGING OF WINDOWS DURING PIV TESTING Meghan R. Luff Advisor: Prof. Christopher P. Goyne The University of Virginia, Charlottesville, VA, 22904 Abstract

DocID: 1phnS - View Document