Presentation is loading. Please wait.

Presentation is loading. Please wait.

AAE 450 Spring 2008 Stephan Shurn 31 January 2008 Propulsion Thrust Vector Control.

Published byVanessa Austin Modified over 9 years ago

Similar presentations

Presentation on theme: "AAE 450 Spring 2008 Stephan Shurn 31 January 2008 Propulsion Thrust Vector Control."— Presentation transcript:

1 AAE 450 Spring 2008 Stephan Shurn 31 January 2008 Propulsion Thrust Vector Control

2 AAE 450 Spring 2008 Liquid Injection Thrust Vector Control (LITVC)  Works for all engines, especially solid and hybrid  Extra weight for plumbing and injectors  Good for flows due to no parts within exhaust stream Propulsion

3 AAE 450 Spring 2008 Gimballing Propulsion Future Work  MAT code testing  Weight and cost data for TVC  More complexity with Solid/Hybrid due to sealing  Flexible seal gimbals for solid/hybrid  Better for liquid due to combustion chamber and nozzle vectoring as a unit

4 AAE 450 Spring 2008 Backup Propulsion

5 AAE 450 Spring 2008 Sources Propulsion  Baxter, A.N., “The Application of Jet-Pumping to Liquid Injection Thrust Vector Control," AIAA Paper, No. 64-231, June 1964  Ciepluch, Carl, “Technology for Low Cost Solid Rocket Boosters,” NASA TM X-67912, November 1971.  “Thrust Vector Control System Study Program,” Vol. I - Rep. TWR-4037- Vol. 1, Thiokol Chemical Corp. (NASA CR-72727), June 15, 1970.

Download ppt "AAE 450 Spring 2008 Stephan Shurn 31 January 2008 Propulsion Thrust Vector Control."

Similar presentations

The Third Law of Motion Section 3.

The Third Law of Motion Section 3.
A method of extracting more power from Internal Combustion Engines

A method of extracting more power from Internal Combustion Engines
Lecture #12 Ehsan Roohi Sharif University of Technology Aerospace Engineering Department 1.

Lecture #12 Ehsan Roohi Sharif University of Technology Aerospace Engineering Department 1.
Liquid Rocket Engine Cycles

Liquid Rocket Engine Cycles
Rocket Engines Liquid Propellant –Mono propellant Catalysts –Bi-propellant Solid Propellant –Grain Patterns Hybrid Nuclear Electric Performance Energy.

Rocket Engines Liquid Propellant –Mono propellant Catalysts –Bi-propellant Solid Propellant –Grain Patterns Hybrid Nuclear Electric Performance Energy.
Thrust E80 Static Motor Test Spring 2009. Forces on a Rocket

Thrust E80 Static Motor Test Spring Forces on a Rocket
Propulsion Systems. Propulsion System A machine that produces thrust to push an object forward The amount of thrust depends on the mass flow through the.

Propulsion Systems. Propulsion System A machine that produces thrust to push an object forward The amount of thrust depends on the mass flow through the.
Hybrid Propulsion System Basics

Hybrid Propulsion System Basics
AAE 450 Spring 2008 Dana Lattibeaudiere February 7, 2008 New Code Developments.

AAE 450 Spring 2008 Dana Lattibeaudiere February 7, 2008 New Code Developments.
Introduction to Hypersonic Propulsion Systems

Introduction to Hypersonic Propulsion Systems
AAE450 Spring 2009 Lander Phase: Hybrid Propulsion System Propulsion System Sizing and Inert Mass Analysis Hopper and Rover Designs for 10kg Payload Hopper.

AAE450 Spring 2009 Lander Phase: Hybrid Propulsion System Propulsion System Sizing and Inert Mass Analysis Hopper and Rover Designs for 10kg Payload Hopper.
AAE450 Spring 2009 100 Gram Lander CATIA Design Communications Group Trans Lunar Phase Group Toy Ball Analysis Lander CATIA Design Joshua Elmshaeuser Communications.

AAE450 Spring Gram Lander CATIA Design Communications Group Trans Lunar Phase Group Toy Ball Analysis Lander CATIA Design Joshua Elmshaeuser Communications.
MaCH – SR1: Increasing T/W Ratio of Engine 5 APR 2005.

MaCH – SR1: Increasing T/W Ratio of Engine 5 APR 2005.
HTPB Fuel Grain Flow Rate, Sizing, and Thrust. Regression Rate Governs Size The faster the solid propellant is burned, the “fatter” the rocket must be.

HTPB Fuel Grain Flow Rate, Sizing, and Thrust. Regression Rate Governs Size The faster the solid propellant is burned, the “fatter” the rocket must be.
Liquid Rocket Engine Injectors

Liquid Rocket Engine Injectors
AAE450 Senior Spacecraft Design Catherine Frey Week 4: February 8 th, 2007 Propulsion Group, Transfer Vehicle Group Transfer Vehicle Combustion Chamber.

AAE450 Senior Spacecraft Design Catherine Frey Week 4: February 8 th, 2007 Propulsion Group, Transfer Vehicle Group Transfer Vehicle Combustion Chamber.
1 Propulsion Overview MAE155A Dr. Nacouzi. 2 Agenda Introduction to Propulsion Propulsion Systems: Liquids, Solids, other Basic Propulsion Performance.

1 Propulsion Overview MAE155A Dr. Nacouzi. 2 Agenda Introduction to Propulsion Propulsion Systems: Liquids, Solids, other Basic Propulsion Performance.
Propulsion MSU 2006 Jeff Rhoads and Terry Ballinger.

Propulsion MSU 2006 Jeff Rhoads and Terry Ballinger.
AAE 450 Spring 2008 Ricky Hinton March 27 th, 2008 Propulsion Group Nozzle, Test Facility (back-up slides)

AAE 450 Spring 2008 Ricky Hinton March 27 th, 2008 Propulsion Group Nozzle, Test Facility (back-up slides)
AAE 450 Spring 2008 Michael Walker January 17 th 2007 Dynamics and Controls Group Contact Control Methods Research, 1-d Corrections.

AAE 450 Spring 2008 Michael Walker January 17 th 2007 Dynamics and Controls Group Contact Control Methods Research, 1-d Corrections.

Similar presentations

Ads by Google