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Stephanie Morris 2/21/08 Propulsion Standard Deviations

Stephanie Morris 2/21/08 Propulsion Standard Deviations. Propulsion Standard Deviations. Using the standard deviation values from the Vanguard report, the standard deviations for the propellant mass of our launch vehicle were estimated. Assumptions: Launch vehicle of LG-CA-DA-DT.

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192 views • 6 slides

Stephanie Morris 2/7/08 Propulsion Modification to Propulsion Code Preliminary MAT Results

Stephanie Morris 2/7/08 Propulsion Modification to Propulsion Code Preliminary MAT Results. Propulsion Code Modification. Assumptions: Maximum Thrust is 44,482 N Molecular Weight of LOX/LH2 is 7 kg/ kmol O/F is 2.6. Credit to Dana Lattibeaudiere for previous MATLAB code. Propulsion.

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212 views • 5 slides

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Stephanie Morris 2/21/08 Propulsion Standard Deviations

Stephanie Morris 2/7/08 Propulsion Modification to Propulsion Code Preliminary MAT Results