'Space propulsion analysis' presentation slideshows

MAE 4262: ROCKETS AND MISSION ANALYSIS

MAE 4262: ROCKETS AND MISSION ANALYSIS. Rocket Equation and Losses September 4, 2012 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. ROCKET EQUATION: IMPORTANT TRENDS. TYPICAL D V MISSION REQUIREMENTS.

355 views • 14 slides

Lunar Lander Propulsion System 100 g, 10 kg and Arbitrary payload cases Thaddaeus Halsmer Thursday, March 12, 2009

Lunar Lander Propulsion System 100 g, 10 kg and Arbitrary payload cases Thaddaeus Halsmer Thursday, March 12, 2009 Propulsion System Sizes, Performance and Power requirements Propulsion system cost estimate Designed 10 kg payload hopper engines

145 views • 8 slides

Dana Lattibeaudiere February 21, 2008 Propulsion Nozzle Design Injectors

174 views • 5 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.

206 views • 5 slides

200g Balloon Launch Parameters

Scott Breitengross Mar 27, 2008 Trajectory group, Delta V, Saturn V, Feasability Determination, 1 kg Final Design Final Presentation. 200g Balloon Launch Parameters. Tables generated from trajectory code output data. Trajectory. ? V Equations.

160 views • 5 slides

140 views • 4 slides