'Maximum thrust' diaporamas de présentation

FADEC

FADEC. What is FADEC? Digital Electronic Controls Design Requirements : Modern Engine Control System Why is FADEC Preferred? A Backgrounder Location of FADEC Electronic Aspects of FADEC How does FADEC work? FADEC : Functions FADEC : Essential Features

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13-1

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MAE 4262: ROCKETS AND MISSION ANALYSIS

MAE 4262: ROCKETS AND MISSION ANALYSIS. Basics of Chemical Rocket Performance Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. Schematic Diagram of a Conventional Liquid Rocket Motor (Figure 11.1 in Sforza). Northrop Grumman: LOX/LH2 Engine.

602 views • 32 slides

MAE 5380: ROCKETS AND MISSION ANALYSIS

MAE 5380: ROCKETS AND MISSION ANALYSIS. Basics of Chemical Rocket Performance Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. Schematic Diagram of a Conventional Liquid Rocket Motor (Figure 11.1 in Sforza). Northrop Grumman: LOX/LH2 Engine.

341 views • 32 slides

T. YOSHIDA , J. OYAMA, T. HIGUCHI, T. ABE and T. HIRAYAMA

ON THE CHARACTERISTICS IMPROVEMENT OF LINEAR SYNCHRONOUS MOTOR WITH HALF-WAVE RECTIFIED SELF EXCITATION. T. YOSHIDA , J. OYAMA, T. HIGUCHI, T. ABE and T. HIRAYAMA Department of Electrical and Electronic Engineering, Nagasaki University, Japan. Abstract.

501 views • 25 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