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Propulsion and Motor characterization and Propellant formula
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Space Station Commander  
Joined: Fri Sep 05, 2008 9:29 pm
Posts: 637 Location: Austin, Texas 
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 Propulsion and Motor characterization and Propellant formula Posted on: Wed May 06, 2009 9:35 pmTeam Discussions on: Propulsion, Nozzle design, Propellant and motor characteristics
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Launch Director  
Joined: Mon Jan 05, 2009 3:51 pm
Posts: 10 Location: Austin
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Posted on: Thu May 07, 2009 5:35 pm Do you have the motor's for the 'Promethean I" Launch?
BMA |
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Space Station Commander
Joined: Fri Sep 05, 2008 9:29 pm
Posts: 637 Location: Austin, Texas
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Posted on: Thu May 07, 2009 6:10 pm Basil
We still need to get the motors. I'll contact J and see if he can send us a few test motors from the Califorina site. Monroe |
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Space Station Commander
Joined: Fri Sep 05, 2008 9:29 pm
Posts: 637 Location: Austin, Texas
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Posted on: Sun Jun 14, 2009 3:21 pm Richard Nakka from SS2S was nice enough to design a KNSU end burner motor for us and We are working on this H-I Class long burn (15sec.) motor for Dave Hein's Quad Pod III.
It's a standard 35%SU 65%KN mixture 6 inches long x 1.5" with a 1/8" nozzle. We will post a drawing on a new webpage with some information about making KNSU motors and some static testing. I just want to try out Richard's design it should be fun. _________________ Today's the day! We go into Space! |
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