Description:
Published: November 13, 2015
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By: Miguel Maya, University of Southern California
Category:
Aerospace Engineering
Hashtags:
#Aerospace #CalPolyPomona #Engineering #liquidfuelengine #liquidpropulsion #NorthropGrumman #Project #Propulsion #Rocket #Rockets #SpaceX #USC
CDR for liquid rocket injector.
1st generation engine of student-run liquid propulsion lab that I helped co-found at USC.
Engine is to have 2000 N of thrust, or ~500 lbf, and a 10 second burn time.