R0X-56 Design. HTPB Fuel Grain Nitrous Oxide Tank Pre-Combustion Chamber Post-Combustion Chamber Graphite Nozzle Helium Reservoir Vessel Electronics Payload.

Slides:

Advertisements

Similar presentations

P07105: Project METEOR - Steel Rocket January 19, Project METEOR Design and Optimization of a Small Scale Rocket for Pico- Satellite Launching Team.

Advertisements

Team Members: Raul Lugo, Kyle Bowerman Mentor: Matthew Summers

Ruby Gomez (Presenter) Gaines Gibson.  Daedalus Astronautics at ASU  Project Purpose  Chemical Properties  Mixing Procedures  Testing Equipment 

36th Annual Frontiers in Education Conference

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

Uncontrolled copy not subject to amendment

MAE 5391: Rocket Propulsion Overview of Propulsion Systems

Autonomous Vehicle Design Florida Tech AIChE 1999 P. Engel, T. McKenney, M. Mensch.

Hybrid Propulsion System Basics

Propellants Dr. Andrew Ketsdever.

HEL pre-design Diego Perini Superconducting solenoid Operation temperature: 4.2 K, current:about 250A, magnetic field: 5 Tesla Cooled by liquid.

Design Goals Saturn V Ariane 4 Pegasus Vanguard Bellerophon ? ? ?

Parth Kumar ME5643: Mechatronics UAV ATTITUDE AND HEADING HOLD SYSTEM.

1 Unit 1 – Material Properties, Structure, Processes, and Design Material property: attribute of a material that is independent of size or shape. Examples:

MaCH – SR1: Increasing T/W Ratio of Engine 5 APR 2005.

Project M.E.T.E.O.R. P07109: Flying Rocket Team Andrew Scarlata, Geoff Cassell, Zack Mott, Garett Pickett, Brian Whitbeck, Luke Cadin, David Hall.

Classic Concept. HTPB Fuel Grain Nitrous Oxide Tank Pre-Combustion Chamber Post-Combustion Chamber Graphite Nozzle Helium Reservoir Vessel Electronics.

University of Utah Unity IV Responsibilities Motor System –Fuel –Nozzle –Ignition Flight Profile Maximum Energy Footprint.

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.

P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David.

P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David.

Rockets 101 AIAA – March 2009 Theory of Rockets Dr. Eric Besnard California State University, Long Beach Project Director, California Launch Vehicle Education.

Identified Company (CompositeX) to manufacture Custom Composite Pressure Vessel ● Working pressure 1000psi ● Holds 8 kg Nitrous Oxide ● 700 cubic inch.

1 Propulsion Overview MAE155A Dr. Nacouzi. 2 Agenda Introduction to Propulsion Propulsion Systems: Liquids, Solids, other Basic Propulsion Performance.

P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David.

AAE 450 Spring 2008 Ricky Hinton March 27 th, 2008 Propulsion Group Nozzle, Test Facility (back-up slides)

Hybrid Rocket Combustion Process & Nozzle John Chambers.

University of Utah Unity IV Responsibilities Motor System –Fuel –Nozzle –Ignition Flight Profile Maximum Energy Footprint.

Rocket Propulsion.

V ERIFICATION OF A F LIGHT R EADY H YBRID R OCKET M OTOR Presenter: Deyzi Ixtabalan Partner: Ryan Stoner Arizona State University.

 The word "rocket" can mean different things. Most people think of a tall, thin, round vehicle. They think of a rocket that launches into space. "Rocket"

Project M.E.T.E.O.R. P07109: Flying Rocket Team Andrew Scarlata, Geoff Cassell, Zack Mott, Garett Pickett, Brian Whitbeck, Luke Cadin, David Hall.

Aerospace fuel and it’s composition

Tropos-1 Hybrid rocket Project

Rocketry Kim Lachler Updated 2015 NCES: Rocketry The Chinese invented the crude gunpowder rockets. The Chinese invented the crude gunpowder rockets.

36th Annual Frontiers in Education Conference

Vacuum Fundamentals 1 atmosphere = 760 mm Hg = kPa 1 torr = 1 mm Hg vacuum range pressure range low 760 ~ 25 torr medium 25~ high ~ 10.

Comprehend the different types of rockets Comprehend the propulsion and flight of rockets Comprehend the types of launch vehicles Comprehend the factors.

The Layers of the Earth Look for patterns in these pictures of the inside of the Earth:

 Expand upon knowledge base developed from Panther 1 solid rocket launch (6/28/06)  Enhance relationship and training opportunities between Florida.

How Rocket Engines Operate List the Types and Characteristics of Rocket Engines How Rockets Work.

HYBRID ROCKET PROPULSION SYSTEMS BY: MCDOG SNIZZY ALLEN A.K.A SHAWN.

Engineering Materials Dr. Berlanty Iskander. Types of Materials.

Analytical and Empirical Characterization of Hybrid Rocket Swirl Injection Presenters: Matt H. Summers Advisor: James K. Villarreal.

Project M.E.T.E.O.R. P07109: Flying Rocket Team

AAE450 Spring 2009 Lunar Lander Main Engine Thaddaeus Halsmer Thursday, February 12, 2009 Thaddaeus Halsmer, Propulsion.

AMCOM MK66 Guidance Module Software Block Diagram Data Handler IMU ProcessingGPS ProcessingRMS Control Serial I/O Ctrl Parallel Ctrl.Actuate,

Effects of Swirl Injector Design on Hybrid Rocket Fuel Regression Rate

8.4 Earth’s Layers. Layers by Composition Earth’s interior consists of three major zones defined by its chemical composition. CrustMantleCore.

Geologist A scientist who studies the Earth as well as the processes and history that have shaped it.

Design of rocket Stages of rocket Design of rocket Three stages design of Saturn V Apollo spaceship 3rd stage rocket 2nd stage rocket 1st stage rocket.

TESLA Rocket Project Lecture #3 10/28/15

Solid Rocket Motors A solid rocket motor is a system that uses solid propellants to produce thrust Advantages High thrust Simple Storability High density.

Aerospace Education - Aircraft Systems 1. 2 Aircraft Powerplants (Engines) 5.

ROCKET CHEMISTRY. SO YOU WANT TO GO TO SPACE? For every action there is an equal and opposite reaction.

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

1 SOLID PROPELLANT ROCKETS Solid fuel rockets rely on controlled explosion of a mixture of substances Nearly a homogeneous material that is burned Similar.

Apex. TRL:# Risk:  Apex has designed a rocket engine to meet the following criteria: Hybrid engine utilizing liquid N 2 O oxidizer Produce between 75.

The Interior Structure of Earth

The Layers of the Earth!.

Oxidizer Tank and Delivery Team

Rocket Engines Liquid Propellant Solid Propellant Hybrid Nuclear

ROCKETS AND MISSION ANALYSIS

Development and Principles of Rocketry

MaCH – SR1: Increasing T/W Ratio of Engine

Shuttle Main Engine LOX System (typical of 3)

Project M.E.T.E.O.R. Flying Rocket Team P07109 Combustion Assembly

John Beasley 3/20/2008 Propulsion Group Contact: Black Boxes and Code Flowchart AAE 450 Spring 2008.

DESIGN OF THE ARIES IV TRIBRID LIQUID PROPELLANT ROCKET ENGINE

APP-3 CHAMBER Insulation DESIGN PROBLEM

Presentation transcript:

R0X-56 Design

HTPB Fuel Grain Nitrous Oxide Tank Pre-Combustion Chamber Post-Combustion Chamber Graphite Nozzle Helium Reservoir Vessel Electronics Payload Micro IMU (Inertial Measurement Unit) Composite Outer Shell (Aluminum Inner Reinforced)

Micro IMU Provides serial digital outputs of tri- axial acceleration, rate of turn (gyro) and tri-axial magnetic field data. Payload Pico-Satellite Electronics Avionics and Data Acquisition Helium Reservoir Vessel – Provides better thrust vectoring because of its smaller molecular weight (compared to NOS). Helium is also less sensitive to extreme temperatures

HTPB Fuel Grain (Solid Fuel) Hybrid Fuel Mixing Zone Pre-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell Note: Components will be wrapped with composite skin to hold them in place. M-NPT Threading Nitrous Oxide Tank (Liquid Fuel)

Pre-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell HTPB Fuel Grain (Solid Fuel) Note: Components will be wrapped with composite skin to hold them in place. Hybrid Fuel Mixing Zone Graphite Nozzle – Currently has the exact specifications as the steel rocket