U S ARMY FOREIGN SCIENCE h AND TECHNOLOGY CENTER. 2KTBRI0R BALLISTICS W TUBE NEAP AND SOLID PROPELLANT ROCKETS (TABLE OF CORTlim) N.B.

Size: px
Start display at page:

Download "U S ARMY FOREIGN SCIENCE h AND TECHNOLOGY CENTER. 2KTBRI0R BALLISTICS W TUBE NEAP AND SOLID PROPELLANT ROCKETS (TABLE OF CORTlim) N.B."

Transcription

1 WTC-HT-25-1S02-71 M U S ARMY FOREIGN SCIENCE h AND TECHNOLOGY CENTER 1 II 2KTBRI0R BALLISTICS W TUBE NEAP AND SOLID PROPELLANT ROCKETS (TABLE OF CORTlim) imt -:.. :~--:-i 3^ ^* :: -k*"4 mam ll;^4 N.B. S*r«bry«kov '- ^ 51#: USSR This dooumnt i» a rtvtdition of tho original foraign taxt uithout cmg CMilgtioal or aditorial eammnt. NATIONAL TECHNICAL i^4for^lation SERVICE '.«>«>«f>«l4.»» Util 'Aff»o««d fiar publk rtbaw; dumrikmioa 'W &

2 ffikmmmnmiww mumim Asama rmttflt tittim OOCUMINT CONTROL DATA «A P tlrnmlt, * UHMhm W MM», *w» rf t«l I «X I^M»M IHHI wmm to mmt i. oiii«j«ti N t ACTivirv ftm^ssmsm) Immmmr memm el»mmmtmm Foreign Seltne«and Taehnology Center US Any Materiel Coanand Department of the kny VnlanitUi ie MOUP Interior Ballistics of Tube Weapons and Solid Propellant Rockets (Table of Contents) 4. MteniPTlvl MOTBt (Tn* InrtHmä imlmlw turn) t rifffliiftim&ssr. muä, UM. gras; M.E. Serebryakov MIPOMT OATI M. CONTRACT ON «HANT NO 3 February 1972 T«. TOTAL NO. Or»*«5 JiZi.» omoinaton*» NBPOMT NUMMMW t. PROJICTMO.,.T * Requester CM Melocik 1». KSTMOUTION TATKMBNT FSTC-HT SK üöwttsr Nora zstztrs* mssss Approved for public release; distribution unlimited. u. iwsnm II.»OMMItlN«MIL!TAUT ACTIVITY US Army Foreign Science and Technology Center The table of contents of a study on the subject of the interior ballistics of tube weapons and solid propellant rockets is given. IMTMM/S eeseatawels»!»*. yum^ify^ r

3 wiiwimiiwk SIFIED 14. LINN Interior Ballistics Solid Rocket Propellant System Gas Dynamics Solid Propellant Combustion Gun Barrel Propellant R and D Propellent Burning Rate SUBJECT CODE: 19 COUNTRY CODE: UR «kl «T NOkl (.IM««LINN C NOLI «T UHCLASSIFTRD

4 TECHNICAL TRANSLATION FSTC-H ENGLISH TITLE: Interior Ballistics of Tube Weapons and Solid Propellant Rocket» (Table of Contents) FOREIGN TITLE: Vnutrennyaya Ballistika Stvol'nykh Sistem i Porokhovykh Raket AUTHOR: M.E. Serebryakov SOURCE: COST, State Scientific and Technical PublisheT«. of Literature on Defense, Moscow, Translated for FSTC by Leo Kanner Associates, Redwood City, Ca. (Eakin) NOTICE The contents o ( this publication have been translated as presented in the original text. No attempt has been made to verify the accuracy of any statement contained herein. This translation is published with a minimum of copy editing and graphics preparation in order to expedite the dissemination of information. Requests for additional copies of this document should be addressed to Department A, National Technical Information Service, Springfield, Virginia Approved for public release; distribution unlimited.

5 CONTENTS Foreword Basic designations Introduction PART ÜNE The Theoretical Basis of Internal Ballistics / Chapter I. Basic facts of thermodynamics 1. Parameters of the gaseous state 2. Equations of the gaseous state 3. Gas mixtures 4. Thermodynamics processes 5. Heat capacity of a gas 6. Internal energy of a gas 7. External work of a gas 8. The law of conservation of energy. The principle of equivalence of heat and work 9. The first law of thermodynamics 10. A method of investigating thermodynamic processes 11. Enthalpy 12. The isobaric process 13. The isotherraic process 14. The adiabatic process 15. The polytropic process 16. Reversible and nonreversible processes 17. The Camot cycle 18. The second law of thermodynamics 19. Concept of entropy Chapter II. Basic principles of gas dynamics The diversity of gas flows Setting up a problem of a one-dimensional gas flow The equation of motion The equation of conservation of mass / -1-

6 MI« The equation of energy 72 A system of equations 76 The equation of quantity of motion 77 The speed of sound 79 The speed of gas flow 80 Critical parameters of the flow 83 The relationship between pressure and cross-section area of a gas stream. Passage of gas in a second 85 The supersonic nozzle 88 Peculiarities of the supersonic nozzle and conditions of its work 92 A nozzle with a sloping cut-off 96 Propulsion force 97 Specific thrust 104 Chapter III. Principles of burning sdid propellants and the formation of gases in a constant volume Solid propel lants and their characteristics. Classification and arrangement of charges Burning of solid propellants Kinetics of burning solid propellants The relationship between pressure and conditions of loading when burning solid propellants irt-i constant volume The theoretical dependence p=f(t) in burning a solid propellant in a constant volume Loss due to heat transfer into the walls when burning , 12. solid propellants in a constant volume 176 The physical law of burning solid propel lant:. 182 Ppculiarities of burning solid propellants with narrow channels 194 Integral diagrams and their application 205 Ballistic analysis of solid propellants through experiments in manometric bombs 216 Peculiarities of burning combined charges 217 Peculiarities of burning solid propellants in a constant volume with the escape of powder gases through a nozzle 228 PART TWO The Peculiarities of Burning Solid Propellant Charges in a Rocket Chamber Chapter IV. Internal ballistics of solid propellant rockets Peculiarities of burning a solid propellant charge in a rocket chamber The form of solid propellant charges Ignition of afcharge in a rocket's chamber Steadiness of charge burning

7 4. 5. Influence of the charge temperature and heat losses in the process of its burning Durability and fragility of a solid propellant charge The mechanism of burning solid rocket fuel. The phenomenon of erosion 8. Solving a problem of internal ballistics for solid propellant rockets 9. Understanding turbo-reactive shells 10. On new types of solid fuels for rockets / PART THREE The Physical Fundamentals of the Phenomenon of Firing from Barrel Systems ' Chapter V. Physical Bases of the process of firing up to the departure of the shell from the bore channel The phenomenon of firing, the basic processes and dependencies [Note: page Researching the basic dependencies in firing numbers not Forces created by the movement of the shell along the given are grooved bore. illegible Secondary reaction of solid propellant gases in firing in the The dependency between pressure on the bottom of the original.] channel and on the bottom of the shell Influence of the shape of the chamber on the process of pressure development 5. Estimate of heat transfer through the walls of the bore in weapons in firing Chapter VI. The period of aftereffects of gas-is on the shell and on the bore Aftereffects of gases on the bore. recoil without muzzle briking Muzzle brakes Aftereffects of gases on the shell The theory of free PART FOUR The Basic Problem of Internal Ballistics and Methods of Its Solution Solving Problems of Internal Ballistics and the Basic Principles of the Process of Firing for Bore Systems iv Chapter VII, Solving the basic problem of internal ballistiöp üy analytical methods 1. Setting up the problem, a system of equations, basic allowances -3-

8 7. 2. The analytical method of solving a basic problem with the geometrical law of burning Solving a problem of internal ballistics for a combined charge Solving a problem of internal ballistics on the basis of the physical law of burning Chapter VIII. Numerical methods, tables, correction formulas. Concepts of the application of electronic digital computers , Numerical methods of solution Tables for solving problems of internal ballistics Basic observations from the theory of similarity Correction formulas of internal ballistics Understanding the solution of a problem of internal ballistics with the aid of rapid-action calculating machines Chapter IX. Basic principles of the process of firing under different loading conditions The case of instant propellant burning Basic dependencies for solid fuel with a constant surface burning for po= Maintaining p max =const, when several loading conditions are changing Influence of change of the burning rate law on the change of several ballistic characteristics in firing The influence of the shape of the powder and its dimensions on the pressure of the gases and the speed of the projectile The influence of the change of forcing pressure PO on the change of the ballistic elements of firing The influence of steady cutting of the band of the shell in the rifling on the ballistics elements of firing 554 Chapter X. Ballistic design of bore systems of the usual type A problem of ballistic design of a bore On* the history of the development of ballistic gun design in the Soviet Union The ballistic characteristics of weapons Theoretical fundamentals of ballistic projection of weapons The development of a method of ballistical design The practice of ballistic calculation Ballistic projection in combined charges Additional information

9 mufmimmmmim. Chapter XI. Peculiarities of certain special types of bore weapons Peculiarities of internal ballistics of firing weapons Peculiarities of internal ballistics in the firing of subcaliber shells Understanding the peculiarities of internal ballistics of bores with conical.channels Ballistic possibilities of solid propellants of a high progresslveness Using light gases for obtaining very high initial speeds 656 Chapter XII. Bore systems with escaping gases during the burning of the propellant Undsrstanding the peculiarities of the internal ballistics of gas-dynamic weapons Peculiarities of internal ballistic non-recoiling weapons (BO) Peculiarities of internal ballistics of mine-throwers 682 Bibliography; To the first part 697 To the second part 697 To the third part 698 To the fourth part 698

Contents. Preface... xvii

Contents. Preface... xvii Contents Preface... xvii CHAPTER 1 Idealized Flow Machines...1 1.1 Conservation Equations... 1 1.1.1 Conservation of mass... 2 1.1.2 Conservation of momentum... 3 1.1.3 Conservation of energy... 3 1.2

More information

Rocket Propulsion. Combustion chamber Throat Nozzle

Rocket Propulsion. Combustion chamber Throat Nozzle Rocket Propulsion In the section about the rocket equation we explored some of the issues surrounding the performance of a whole rocket. What we didn t explore was the heart of the rocket, the motor. In

More information

Richard Nakka's Experimental Rocketry Web Site

Richard Nakka's Experimental Rocketry Web Site Página 1 de 7 Richard Nakka's Experimental Rocketry Web Site Solid Rocket Motor Theory -- Nozzle Theory Nozzle Theory The rocket nozzle can surely be described as the epitome of elegant simplicity. The

More information

CONTENTS Real chemistry e ects Scramjet operating envelope Problems

CONTENTS Real chemistry e ects Scramjet operating envelope Problems Contents 1 Propulsion Thermodynamics 1-1 1.1 Introduction.................................... 1-1 1.2 Thermodynamic cycles.............................. 1-8 1.2.1 The Carnot cycle.............................

More information

Applied Thermodynamics - II

Applied Thermodynamics - II Gas Turbines Sudheer Siddapureddy sudheer@iitp.ac.in Department of Mechanical Engineering Jet Propulsion - Classification 1. A heated and compressed atmospheric air, mixed with products of combustion,

More information

A GAS DYNAMICS BASED METHOD FOR ARTILLERY INTERIOR BALLISTICS DEDICATED TO NEW PROPULSIVE CHARGES DESIGN

A GAS DYNAMICS BASED METHOD FOR ARTILLERY INTERIOR BALLISTICS DEDICATED TO NEW PROPULSIVE CHARGES DESIGN A GAS DYNAMICS BASED METHOD FOR ARTILLERY INTERIOR BALLISTICS DEDICATED TO NEW PROPULSIVE CHARGES DESIGN LIVIU MATACHE MARIUS VALERIU CÎRMACI MATEI ADRIAN NICOLAE ROTARIU NISTORAN GEORGETA DIANA Faculty

More information

'IU.S. . I..'...p i I - I I I ';; - : = : - Ott ARMY , FOREIGN SCIENCE AND TECHNOLOGY CENTER. JUN Subject Country: USSR zr1~up

'IU.S. . I..'...p i I - I I I ';; - : = : - Ott ARMY , FOREIGN SCIENCE AND TECHNOLOGY CENTER. JUN Subject Country: USSR zr1~up -s- - - FSTC,NT-23-123-72 'IU.S. ARMY MATERIEL COMMAND ARMY, FOREIGN SCIENCE AND TECHNOLOGY CENTER Ott AI A NATURAL INITIAL SOLUTION AND SENSITIVITY ANALYSIS OF THE OPTIMUM SOLUTION IN LINEAR PROGRAMMI-1C

More information

FFI/RAPPORT-2006/03004

FFI/RAPPORT-2006/03004 FFI RAPPORT Studies of wear characteristics of three different gunpowder gases FRØYLAND ØYVIND, MOXNES JOHN F. FFI/RAPPORT-2006/03004 Studies of wear characteristics of three different gunpowder gases

More information

Solid Rocket Motor Internal Ballistics Using a. Least-Distance Surface-Regression Method

Solid Rocket Motor Internal Ballistics Using a. Least-Distance Surface-Regression Method 23 rd ICDERS July 24-29, 211 Irvine, USA Solid Rocket Motor Internal Ballistics Using a Least-Distance Surface-Regression Method C. H. Chiang Department of Mechanical and Automation Engineering I-Shou

More information

PROPULSIONE SPAZIALE. Chemical Rocket Propellant Performance Analysis

PROPULSIONE SPAZIALE. Chemical Rocket Propellant Performance Analysis Chemical Rocket Propellant Performance Analysis Sapienza Activity in ISP-1 Program 15/01/10 Pagina 1 REAL NOZZLES Compared to an ideal nozzle, the real nozzle has energy losses and energy that is unavailable

More information

COMPARISON OF 0D AND 1D INTERIOR BALLISTIC MODELLING OF HIGH PERFORMANCE DIRECT FIRE GUNS C. R.

COMPARISON OF 0D AND 1D INTERIOR BALLISTIC MODELLING OF HIGH PERFORMANCE DIRECT FIRE GUNS C. R. IB06 19th International Symposium of Ballistics, 7 11 May 2001, Interlaken, Switzerland COMPARISON OF 0D AND 1D INTERIOR BALLISTIC MODELLING OF HIGH PERFORMANCE DIRECT FIRE GUNS C. R. Woodley WS4 Guns

More information

Technology of Rocket

Technology of Rocket Technology of Rocket Parts of Rocket There are four major parts of rocket Structural system Propulsion system Guidance system Payload system Structural system The structural system of a rocket includes

More information

EFFECT OF INCREASE IN STARTING PRESSURE ON EFFICIENCY AND VELOCITY OF CALIBER 0.30 WEAPONS

EFFECT OF INCREASE IN STARTING PRESSURE ON EFFICIENCY AND VELOCITY OF CALIBER 0.30 WEAPONS AD 701 867 EFFECT OF INCREASE IN STARTING PRESSURE ON EFFICIENCY AND VELOCITY OF CALIBER 0.30 WEAPONS H. P. Hitchcock Ballistic Research Laboratories Aberdeen Proving Ground, Maryland 28 July 1941 OlttrlbHtf

More information

GAS DYNAMICS. M. Halük Aksel. O. Cahit Eralp. and. Middle East Technical University Ankara, Turkey

GAS DYNAMICS. M. Halük Aksel. O. Cahit Eralp. and. Middle East Technical University Ankara, Turkey GAS DYNAMICS M. Halük Aksel and O. Cahit Eralp Middle East Technical University Ankara, Turkey PRENTICE HALL f r \ New York London Toronto Sydney Tokyo Singapore; \ Contents Preface xi Nomenclature xiii

More information

AAE COMBUSTION AND THERMOCHEMISTRY

AAE COMBUSTION AND THERMOCHEMISTRY 5. COMBUSTIO AD THERMOCHEMISTRY Ch5 1 Overview Definition & mathematical determination of chemical equilibrium, Definition/determination of adiabatic flame temperature, Prediction of composition and temperature

More information

PRESSURE DISTRIBUTION IN THE SPACE BEHIND A PROJECTILE

PRESSURE DISTRIBUTION IN THE SPACE BEHIND A PROJECTILE Advances in MT PRESSURE DISTRIBUTION IN THE SPACE BEHIND A PROJECTILE 35 Luděk JEDLIČKA Stanislav BEER PRESSURE DISTRIBUTION IN THE SPACE BEHIND A PROJECTILE Reviewer: Bohumil PLÍHAL Abstract: This article

More information

Jet Propulsion. Lecture Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati

Jet Propulsion. Lecture Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati Lecture - 27 Prepared under QIP-CD Cell Project Jet Propulsion Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1 Propellant Properties High specific impulse

More information

SOLID ROCKET MOTOR INTERNAL BALLISTICS SIMULATION USING DIFFERENT BURNING RATE MODELS

SOLID ROCKET MOTOR INTERNAL BALLISTICS SIMULATION USING DIFFERENT BURNING RATE MODELS U.P.B. Sci. Bull., Series D, Vol. 76, Iss. 4, 2014 ISSN 1454-2358 SOLID ROCKET MOTOR INTERNAL BALLISTICS SIMULATION USING DIFFERENT BURNING RATE MODELS Marius Ionuţ MĂRMUREANU 1 The burning rate of solid

More information

A THEORETICAL METHOD OF PROPELLANTS BALLISTIC PARAMETERS CALCULUS

A THEORETICAL METHOD OF PROPELLANTS BALLISTIC PARAMETERS CALCULUS A THEORETICAL METHOD OF PROPELLANTS BALLISTIC PARAMETERS CALCULUS LIVIU-CRISTIAN MATACHE 1,2 TEODORA ZECHERU 1 CONSTANTIN ENACHE 2 ADRIAN ROTARIU 2 EUGEN TRANĂ 2 Abstract: The present study aims at achieving

More information

First Law of Thermodynamics

First Law of Thermodynamics CH2303 Chemical Engineering Thermodynamics I Unit II First Law of Thermodynamics Dr. M. Subramanian 07-July-2011 Associate Professor Department of Chemical Engineering Sri Sivasubramaniya Nadar College

More information

Matter exchange - type of wall Yes - permeable - absence of wall. Energy exchange - type of wall. - diathermic - moving wall. Yes

Matter exchange - type of wall Yes - permeable - absence of wall. Energy exchange - type of wall. - diathermic - moving wall. Yes I. The concept of work, expansion and additional (useful) work. II. The concept of heat. III. Definition of internal energy and its molecular interpretation. I. Different forms of the first law of thermodynamics..

More information

UNIFIED ENGINEERING Fall 2003 Ian A. Waitz

UNIFIED ENGINEERING Fall 2003 Ian A. Waitz Ian A. Waitz Problem T6. (Thermodynamics) Consider the following thermodynamic cycle. Assume all processes are quasi-static and involve an ideal gas. 3 p Const. volume heat addition 2 adiabatic expansion

More information

UNCLASSIFIED AD NUMBER LIMITATION CHANGES

UNCLASSIFIED AD NUMBER LIMITATION CHANGES TO: UNCLASSIFIED AD NUMBER AD240143 LIMITATION CHANGES Approved for public release; distribution is unlimited. FROM: Distribution authorized to U.S. Gov't. agencies and their contractors; Administrative/Operational

More information

Contents. 1 Introduction to Gas-Turbine Engines Overview of Turbomachinery Nomenclature...9

Contents. 1 Introduction to Gas-Turbine Engines Overview of Turbomachinery Nomenclature...9 Preface page xv 1 Introduction to Gas-Turbine Engines...1 Definition 1 Advantages of Gas-Turbine Engines 1 Applications of Gas-Turbine Engines 3 The Gas Generator 3 Air Intake and Inlet Flow Passage 3

More information

Contents. 2 Basic Components Aerofoils Force Generation Performance Parameters xvii

Contents. 2 Basic Components Aerofoils Force Generation Performance Parameters xvii Contents 1 Working Principles... 1 1.1 Definition of a Turbomachine... 1 1.2 Examples of Axial Turbomachines... 2 1.2.1 Axial Hydraulic Turbine... 2 1.2.2 Axial Pump... 4 1.3 Mean Line Analysis... 5 1.4

More information

fla'

fla' -Mt43 914 T-NOTOR TESTS WITH CYLINDRICAL ORRXNS(U FOuEIhh In TECHNOLOGY DIV HRIOHT-PRTTERSON MY OH K YEN IS JUL. 64 FT-IDCRtS)T-S779-9 UNCLRSSIFXED Ft'S 21/. 2 N EEEmiEEEEEmi * -.. *..- -- *. ~ - -*.,.-..

More information

Stochastic study of 60-mm gun-projectile responses

Stochastic study of 60-mm gun-projectile responses Computational Ballistics III 77 Stochastic study of 60-mm gun-projectile responses M. Chen Army Research Laboratory, USA Abstract Gun propulsion modeling has been under development for many decades. Starting

More information

Rifles In-Bore Finite Element Transient Analysis

Rifles In-Bore Finite Element Transient Analysis Rifles In-Bore Finite Element Transient Analysis S. Deng, H. K. Sun, and Chung-Jung Chiu Abstract This research used nonlinear transient Finite element method to simulate 5.56 mm rifle bullet s behavior

More information

CHEM Thermodynamics. Work. There are two ways to change the internal energy of a system:

CHEM Thermodynamics. Work. There are two ways to change the internal energy of a system: There are two ways to change the internal energy of a system: Thermodynamics Work 1. By flow of heat, q Heat is the transfer of thermal energy between and the surroundings 2. By doing work, w Work can

More information

Design and Optimization of De Lavel Nozzle to Prevent Shock Induced Flow Separation

Design and Optimization of De Lavel Nozzle to Prevent Shock Induced Flow Separation Advances in Aerospace Science and Applications. ISSN 2277-3223 Volume 3, Number 2 (2013), pp. 119-124 Research India Publications http://www.ripublication.com/aasa.htm Design and Optimization of De Lavel

More information

Contents. I Introduction 1. Preface. xiii

Contents. I Introduction 1. Preface. xiii Contents Preface xiii I Introduction 1 1 Continuous matter 3 1.1 Molecules................................ 4 1.2 The continuum approximation.................... 6 1.3 Newtonian mechanics.........................

More information

LINEAR MOMENTUM AND COLLISIONS

LINEAR MOMENTUM AND COLLISIONS LINEAR MOMENTUM AND COLLISIONS Chapter 9 Units of Chapter 9 Linear Momentum Momentum and Newton s Second Law Impulse Conservation of Linear Momentum Inelastic Collisions Elastic Collisions Center of Mass

More information

4.1 LAWS OF MECHANICS - Review

4.1 LAWS OF MECHANICS - Review 4.1 LAWS OF MECHANICS - Review Ch4 9 SYSTEM System: Moving Fluid Definitions: System is defined as an arbitrary quantity of mass of fixed identity. Surrounding is everything external to this system. Boundary

More information

The application of nano aluminum powder on solid propellant

The application of nano aluminum powder on solid propellant The application of nano aluminum powder on solid propellant Metal incendiary agent is one of the important components of modern solid propellant, which can improve the explosion heat and density of propellant.

More information

Rocket Thermodynamics

Rocket Thermodynamics Rocket Thermodynamics PROFESSOR CHRIS CHATWIN LECTURE FOR SATELLITE AND SPACE SYSTEMS MSC UNIVERSITY OF SUSSEX SCHOOL OF ENGINEERING & INFORMATICS 25 TH APRIL 2017 Thermodynamics of Chemical Rockets ΣForce

More information

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, IIT Bombay Module No. # 01 Lecture No. # 08 Cycle Components and Component

More information

YUsend-1 Solid Propellant Microthruster Design, Fabrication and Testing

YUsend-1 Solid Propellant Microthruster Design, Fabrication and Testing YUsend-1 Solid Propellant Microthruster Design, Fabrication and Testing 24 th AIAA/USU Conference on Small Satellites Authors: Kartheephan Sathiyanathan, Regina Lee, Hugh Chesser (York University) Charles

More information

COMMITMENT. &SOLUTIONS Act like someone s life depends on what we do. UNPARALLELED

COMMITMENT. &SOLUTIONS Act like someone s life depends on what we do. UNPARALLELED Characterization of Machine Gun Barrel Temperature and Stress Conditions Through Correlation of Testing and Numerical Methods Presented at: NDIA Armament Systems Forum Indianapolis, IN May 2018 UNPARALLELED

More information

IX. COMPRESSIBLE FLOW. ρ = P

IX. COMPRESSIBLE FLOW. ρ = P IX. COMPRESSIBLE FLOW Compressible flow is the study of fluids flowing at speeds comparable to the local speed of sound. This occurs when fluid speeds are about 30% or more of the local acoustic velocity.

More information

SEM-2016(03)-II MECHANICAL ENGINEERING. Paper -11. Please read each of the following instructions carefully before. attempting questions.

SEM-2016(03)-II MECHANICAL ENGINEERING. Paper -11. Please read each of the following instructions carefully before. attempting questions. Roll No. Candidate should write his/her Roll No. here. Total No. of Questions : 7 No. of Printed Pages : 8 SEM-2016(03)-II MECHANICAL ENGINEERING Paper -11 Time : 3 Hours ] [ Total Marks : 300 Instructions

More information

An Introduction to Chemical Kinetics

An Introduction to Chemical Kinetics An Introduction to Chemical Kinetics Michel Soustelle WWILEY Table of Contents Preface xvii PART 1. BASIC CONCEPTS OF CHEMICAL KINETICS 1 Chapter 1. Chemical Reaction and Kinetic Quantities 3 1.1. The

More information

Preface Acknowledgments Nomenclature

Preface Acknowledgments Nomenclature CONTENTS Preface Acknowledgments Nomenclature page xv xvii xix 1 BASIC CONCEPTS 1 1.1 Overview 1 1.2 Thermodynamic Systems 3 1.3 States and Properties 4 1.3.1 State of a System 4 1.3.2 Measurable and Derived

More information

LAWS OF MOTION Newtons laws of motion. (i) First law: Law of inertia. Every body continues to be in its state of rest or of uniform motion in a

LAWS OF MOTION Newtons laws of motion. (i) First law: Law of inertia. Every body continues to be in its state of rest or of uniform motion in a LAWS OF MOTION Newtons laws of motion. (i) First law: Law of inertia. Every body continues to be in its state of rest or of uniform motion in a straight line unless compelled to change that state by an

More information

FUNDAMENTALS OF GAS DYNAMICS

FUNDAMENTALS OF GAS DYNAMICS FUNDAMENTALS OF GAS DYNAMICS Second Edition ROBERT D. ZUCKER OSCAR BIBLARZ Department of Aeronautics and Astronautics Naval Postgraduate School Monterey, California JOHN WILEY & SONS, INC. Contents PREFACE

More information

3. Write a detailed note on the following thrust vector control methods:

3. Write a detailed note on the following thrust vector control methods: Code No: R05322103 Set No. 1 1. Starting from the first principles and with the help of neatly drawn velocity triangles obtain the following relationship: Ψ = 2 Φ (tan β 2 + tan β 3 ) where Ψ is the blade

More information

UNIT 1 COMPRESSIBLE FLOW FUNDAMENTALS

UNIT 1 COMPRESSIBLE FLOW FUNDAMENTALS UNIT 1 COMPRESSIBLE FLOW FUNDAMENTALS 1) State the difference between compressible fluid and incompressible fluid? 2) Define stagnation pressure? 3) Express the stagnation enthalpy in terms of static enthalpy

More information

Chapter 1 Introduction and Basic Concepts

Chapter 1 Introduction and Basic Concepts Chapter 1 Introduction and Basic Concepts 1-1 Thermodynamics and Energy Application Areas of Thermodynamics 1-2 Importance of Dimensions and Units Some SI and English Units Dimensional Homogeneity Unity

More information

MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING. EMEC 426 Thermodynamics of Propulsion Systems. Spring 2017

MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING. EMEC 426 Thermodynamics of Propulsion Systems. Spring 2017 MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING EMEC 426 Thermodynamics of Propulsion Systems Spring 2017 Instructor: Dr. Alan H. George Office: Roberts 119 Office Hours: to be announced

More information

PROPULSION LAB MANUAL

PROPULSION LAB MANUAL PROPULSION LAB MANUAL Measurement of Calorific Value of a Solid Fuel Sample using a Bomb Calorimeter DEPARTMENT OF AEROSPACE ENGINEERING Indian Institute of Technology Kharagpur CONTENTS 1. Introduction

More information

Departures from Ideal Performance for Conical Nozzles and Bell Nozzles, Straight-Cut Throats and Rounded Throats Charles E. Rogers

Departures from Ideal Performance for Conical Nozzles and Bell Nozzles, Straight-Cut Throats and Rounded Throats Charles E. Rogers Departures from Ideal Performance for Conical Nozzles and Bell Nozzles, Straight-Cut Throats and Rounded Throats Charles E. Rogers This article covers departures from ideal performance for conical nozzles

More information

END AD AOSI 255 COLD REGIONS RESEARCH MG ENGINEERING LAB HANOVFR N H F/6.13/2 EVALUATION ~~

END AD AOSI 255 COLD REGIONS RESEARCH MG ENGINEERING LAB HANOVFR N H F/6.13/2 EVALUATION ~~ AD AOSI 255 COLD REGIONS RESEARCH MG ENGINEERING LAB HANOVFR N H F/6.13/2 EVALUATION ~~ STABILITY OF EARTH FILL DAM BASED ON STRENGTH OV ETC(U) JLA 77 6 I KUZNETSOV UNCLASSIFIED CRREL TL 628 ML END DAT

More information

Defense Technical Information Center Compilation Part Notice ADP023640

Defense Technical Information Center Compilation Part Notice ADP023640 UNCLASSIFIED Defense Technical Information Center Compilation Part Notice ADP023640 TITLE: Plasma-Propellant Interaction Studies DISTRIBUTION: Approved for public release, distribution unlimited This paper

More information

New Extended Range Shoulder-Fired 40 mm Grenade System

New Extended Range Shoulder-Fired 40 mm Grenade System New Shoulder-Fired Grenade System Danie Els a Hennie Pieterse b Marius de Bruin c a Dept of Mech and Mechatronics Eng, Univ of Stellenbosch, South Africa dnjels@sun.ac.za b Rippel Effect Weapon Systems

More information

US ARMY FIELD ARTILLERY SCHOOL

US ARMY FIELD ARTILLERY SCHOOL SUBCOURSE FA9011 EDITION A US ARMY FIELD ARTILLERY SCHOOL BALLISTICS TABLE OF CONTENTS Table of Contents... i Instructions... ii Subcourse Overview... iii Lesson 1: Identify the Elements of Interior Ballistics...

More information

PHYSICAL VAPOR DEPOSITION OF THIN FILMS

PHYSICAL VAPOR DEPOSITION OF THIN FILMS PHYSICAL VAPOR DEPOSITION OF THIN FILMS JOHN E. MAHAN Colorado State University A Wiley-Interscience Publication JOHN WILEY & SONS, INC. New York Chichester Weinheim Brisbane Singapore Toronto CONTENTS

More information

MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING. EMEC 426 Thermodynamics of Propulsion Systems. Spring 2018

MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING. EMEC 426 Thermodynamics of Propulsion Systems. Spring 2018 MONTANA STATE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING EMEC 426 Thermodynamics of Propulsion Systems Spring 2018 Instructor: Dr. Alan H. George Office: Roberts 119 Office Hours: to be announced

More information

Rockets, Missiles, and Spacecrafts

Rockets, Missiles, and Spacecrafts 36 1 Rockets, Missiles, and Spacecrafts 2 Chinese used rockets in the 12 th century AD against the Mongol attacks. In India Tipu Sultan used rockets against the British army in the 18 th century. The modern

More information

Section 4.1: Introduction to Jet Propulsion. MAE Propulsion Systems II

Section 4.1: Introduction to Jet Propulsion. MAE Propulsion Systems II Section 4.1: Introduction to Jet Propulsion Jet Propulsion Basics Squeeze Bang Blow Suck Credit: USAF Test Pilot School 2 Basic Types of Jet Engines Ramjet High Speed, Supersonic Propulsion, Passive Compression/Expansion

More information

AAE SOLID ROCKET PROPULSION (SRP) SYSTEMS

AAE SOLID ROCKET PROPULSION (SRP) SYSTEMS 7. SOLID ROCKET PROPULSION (SRP) SYSTEMS Ch7 1 7.1 INTRODUCTION 7.1 INTRODUCTION Ch7 2 APPLICATIONS FOR SRM APPLICATIONS FOR SRM Strap-On Boosters for Space Launch Vehicles, Upper Stage Propulsion System

More information

DEPARTMENT OP THE ARMY V.*. ARMY FORKION SCIENCK AND TCCHNOLOOV CKNTCR UO SCVCNTH STRKCr NK. CHARLOTTESVIIXC, VIRGINIA UNI TRANSLATION

DEPARTMENT OP THE ARMY V.*. ARMY FORKION SCIENCK AND TCCHNOLOOV CKNTCR UO SCVCNTH STRKCr NK. CHARLOTTESVIIXC, VIRGINIA UNI TRANSLATION i i - üiüi rtimmi,...j*!.. -. l w, DEPARTMENT OP THE ARMY V.*. ARMY FORKION SCIENCK AND TCCHNOLOOV CKNTCR UO SCVCNTH STRKCr NK. CHARLOTTESVIIXC, VIRGINIA UNI 10 o 00 In Reply Refer to: FSTC HT-23-836-72

More information

Department of Mechanical Engineering BM 7103 FUELS AND COMBUSTION QUESTION BANK UNIT-1-FUELS

Department of Mechanical Engineering BM 7103 FUELS AND COMBUSTION QUESTION BANK UNIT-1-FUELS Department of Mechanical Engineering BM 7103 FUELS AND COMBUSTION QUESTION BANK UNIT-1-FUELS 1. Define the term fuels. 2. What are fossil fuels? Give examples. 3. Define primary fuels. Give examples. 4.

More information

PROPELLANT-DRIVEN MAGNETIC FLUX COMPRESSION GENERATOR. Pharis E. Williams. Abstract

PROPELLANT-DRIVEN MAGNETIC FLUX COMPRESSION GENERATOR. Pharis E. Williams. Abstract AN INTRODUCTION TO THE PROPELLANT-DRIVEN MAGNETIC FLUX COMPRESSION GENERATOR Pharis E. Williams Abstract An introduction to the concept of a propellant-driven magnetic flux compression generator is presented,

More information

Fundamentals of explosive chemistry. Synopsis:

Fundamentals of explosive chemistry. Synopsis: Fundamentals of explosive chemistry Synopsis: This book is used as a textbook for Ammunition Technical Officers Course and Artillery Course in Chemistry Department, Faculty of Science, Universiti Teknologi

More information

Engineering Thermodynamics

Engineering Thermodynamics Basic Engineering Thermodynamics A Venkatesh Professor Emeritus, Mechanical Engineering Department East West Institute of Technology, Bangalore, India (Formerly Professor of Mechanical Engineering, IIT

More information

CHALLENGES OF INTERNAL BALLISTICS MODELLING OF NOVEL PROPELLANTS AND PROPELLANT GEOMETRY

CHALLENGES OF INTERNAL BALLISTICS MODELLING OF NOVEL PROPELLANTS AND PROPELLANT GEOMETRY 23 RD INTERNATIONAL SYMPOSIUM ON BALLISTICS TARRAGONA, SPAIN 16-20 APRIL 2007 CHALLENGES OF INTERNAL BALLISTICS MODELLING OF NOVEL PROPELLANTS AND PROPELLANT GEOMETRY M. Pocock 1, S. Einstein 2 C. Guyott

More information

Injection and Combustion Principles at Rocket Conditions Malissa Lightfoot, Stephen Danczyk and Venke Sankaran

Injection and Combustion Principles at Rocket Conditions Malissa Lightfoot, Stephen Danczyk and Venke Sankaran Injection and Combustion Principles at Rocket Conditions Malissa Lightfoot, Stephen Danczyk and Venke Sankaran Air Force Research Laboratory, Edwards AFB, CA AFTC/PA clearance No. 15013, 16 January 2015

More information

1. For an ideal gas, internal energy is considered to be a function of only. YOUR ANSWER: Temperature

1. For an ideal gas, internal energy is considered to be a function of only. YOUR ANSWER: Temperature CHAPTER 11 1. For an ideal gas, internal energy is considered to be a function of only. YOUR ANSWER: Temperature 2.In Equation 11.7 the subscript p on the partial derivative refers to differentiation at

More information

BOUNDARY LAYER MODELLING OF THE HEAT TRANSFER PROCESSES FROM IGNITERS TO ENERGETIC MATERIALS Clive Woodley, Mike Taylor, Henrietta Wheal

BOUNDARY LAYER MODELLING OF THE HEAT TRANSFER PROCESSES FROM IGNITERS TO ENERGETIC MATERIALS Clive Woodley, Mike Taylor, Henrietta Wheal 23 RD INTERNATIONAL SYMPOSIUM ON BALLISTICS TARRAGONA, SPAIN 16-20 APRIL 2007 BOUNDARY LAYER MODELLING OF THE HEAT TRANSFER PROCESSES FROM IGNITERS TO ENERGETIC MATERIALS Clive Woodley, Mike Taylor, Henrietta

More information

ONE DIMENSIONAL ANALYSIS PROGRAM FOR SCRAMJET AND RAMJET FLOWPATHS

ONE DIMENSIONAL ANALYSIS PROGRAM FOR SCRAMJET AND RAMJET FLOWPATHS ONE DIMENSIONAL ANALYSIS PROGRAM FOR SCRAMJET AND RAMJET FLOWPATHS Kathleen Tran and Walter F. O'Brien, Jr Center for Turbomachinery and Propulsion Research Virginia Polytechnic Institute and State University

More information

Compressible Flow. Professor Ugur GUVEN Aerospace Engineer Spacecraft Propulsion Specialist

Compressible Flow. Professor Ugur GUVEN Aerospace Engineer Spacecraft Propulsion Specialist Compressible Flow Professor Ugur GUVEN Aerospace Engineer Spacecraft Propulsion Specialist What is Compressible Flow? Compressible Flow is a type of flow in which the density can not be treated as constant.

More information

Numerical Simulation of Flow in a Solid Rocket Motor: Combustion Coupled with Regressive Boundary

Numerical Simulation of Flow in a Solid Rocket Motor: Combustion Coupled with Regressive Boundary Numerical Simulation of Flow in a Solid Rocket Motor: Combustion Coupled with Regressive Boundary Mehmet Özer Havlucu Department of Mechanical Engineering Istanbul Technical University Istanbul, Turkey

More information

Thermodynamic system is classified into the following three systems. (ii) Closed System It exchanges only energy (not matter) with surroundings.

Thermodynamic system is classified into the following three systems. (ii) Closed System It exchanges only energy (not matter) with surroundings. 1 P a g e The branch of physics which deals with the study of transformation of heat energy into other forms of energy and vice-versa. A thermodynamical system is said to be in thermal equilibrium when

More information

On Analogy of 2D and 3D Combustible Mixture Flows

On Analogy of 2D and 3D Combustible Mixture Flows 25 th ICDERS August 2 7, 2015 Leeds, UK On Analogy of 2D and 3D Combustible Mixture Flows Vladimir A. Levin 1, Ivan S. Manuylovich 1, Vladimir V. Markov 1 1 Institute of mechanics of the Moscow State University,

More information

ONE-DIMENSIONAL TWO-PHASE CONSTANT LAO FOW IN COMBUSTION CHAMBER 0F 50.U) FOREION TECHNOLG 00 IV AD-A

ONE-DIMENSIONAL TWO-PHASE CONSTANT LAO FOW IN COMBUSTION CHAMBER 0F 50.U) FOREION TECHNOLG 00 IV AD-A % AD-A145 679 ONE-DIMENSIONAL TWO-PHASE CONSTANT LAO FOW IN COMBUSTION CHAMBER 0F 50.U) FOREION TECHNOLG 00 IV WRIOHT-PATTERSON SFB OH C HSIEN CHR 15 AUG 64 UNCLASSIFE FTD0 ORS)0860-84 F/G212 N 1 1-4 11.

More information

Please welcome for any correction or misprint in the entire manuscript and your valuable suggestions kindly mail us

Please welcome for any correction or misprint in the entire manuscript and your valuable suggestions kindly mail us Problems of Practices Of Fluid Mechanics Compressible Fluid Flow Prepared By Brij Bhooshan Asst. Professor B. S. A. College of Engg. And Technology Mathura, Uttar Pradesh, (India) Supported By: Purvi Bhooshan

More information

Review of Fundamentals - Fluid Mechanics

Review of Fundamentals - Fluid Mechanics Review of Fundamentals - Fluid Mechanics Introduction Properties of Compressible Fluid Flow Basics of One-Dimensional Gas Dynamics Nozzle Operating Characteristics Characteristics of Shock Wave A gas turbine

More information

Steven W. Van Sciver. Helium Cryogenics. Second Edition. 4) Springer

Steven W. Van Sciver. Helium Cryogenics. Second Edition. 4) Springer Steven W. Van Sciver Helium Cryogenics Second Edition 4) Springer Contents 1 Cryogenic Principles and Applications 1 1.1 Temperature Scale 2 1.2 Historical Background 4 1.3 Applications for Cryogenics

More information

CHEMICAL THERMODYNAMICS

CHEMICAL THERMODYNAMICS CHEMICAL THERMODYNAMICS Basic Theory and Methods Sixth Edition IRVING M. KLOTZ Morrison Professor Emeritus Northwestern University ROBERT M. ROSENBERG MacMillen Professor Emeritus Lawrence University Visiting

More information

Interior ballistic two-phase flow model of guided-projectile gun system utilizing stick propellant charge

Interior ballistic two-phase flow model of guided-projectile gun system utilizing stick propellant charge Mahmoud Rashad, Xiaobing Interior ballistic two-phase flow model of guided-projectile gun system utilizing stick propellant charge MAHMOUD RASHAD School of Energy and Power Engineering Nanjing University

More information

Altitude Dependence of Rocket Motor Performance

Altitude Dependence of Rocket Motor Performance KIMBERLY ALBANESE, MARY MEYERS, KASSANDRA PRUSKO, AND MICHAEL COURTNEY United States Air Force Academy, 1 2354 Fairchild Drive, USAF Academy, CO, 80840 Michael.Courtney@usafa.edu Abstract: It is well known

More information

AEROSPACE ENGINEERING DEPARTMENT. Second Year - Second Term ( ) Fluid Mechanics & Gas Dynamics

AEROSPACE ENGINEERING DEPARTMENT. Second Year - Second Term ( ) Fluid Mechanics & Gas Dynamics AEROSPACE ENGINEERING DEPARTMENT Second Year - Second Term (2008-2009) Fluid Mechanics & Gas Dynamics Similitude,Dimensional Analysis &Modeling (1) [7.2R*] Some common variables in fluid mechanics include:

More information

Chapter Two. Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency. Laith Batarseh

Chapter Two. Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency. Laith Batarseh Chapter Two Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency Laith Batarseh The equation of continuity Most analyses in this book are limited to one-dimensional steady flows where the velocity

More information

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof A M Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof A M Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Jet Aircraft Propulsion Prof. Bhaskar Roy Prof A M Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Module No. #01 Lecture No. # 07 Jet Engine Cycles For Aircraft propulsion

More information

Prediction of Transient Deflector Plate Temperature During Rocket Plume Impingment and its Validation through Experiments

Prediction of Transient Deflector Plate Temperature During Rocket Plume Impingment and its Validation through Experiments Prediction of Transient Deflector Plate Temperature During Rocket Plume Impingment and its Validation through Experiments PRIYA KAMESH KAMATCHI*, VISHNU POOVIAH*, PISHARADY.J.C ** *Department of Mechanical

More information

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES Chapter 10 THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES It is not the sun to overtake the moon, nor doth the night outstrip theday.theyfloateachinanorbit. The Holy Qur-ān In many engineering applications,

More information

1. (a) Describe the difference between over-expanded, under-expanded and ideallyexpanded

1. (a) Describe the difference between over-expanded, under-expanded and ideallyexpanded Code No: R05322106 Set No. 1 1. (a) Describe the difference between over-expanded, under-expanded and ideallyexpanded rocket nozzles. (b) While on its way into orbit a space shuttle with an initial mass

More information

Chapter 9. Linear Momentum and Collisions

Chapter 9. Linear Momentum and Collisions Chapter 9 Linear Momentum and Collisions Momentum Analysis Models Force and acceleration are related by Newton s second law. When force and acceleration vary by time, the situation can be very complicated.

More information

Introduction to Chemical Engineering Thermodynamics. Chapter 7. KFUPM Housam Binous CHE 303

Introduction to Chemical Engineering Thermodynamics. Chapter 7. KFUPM Housam Binous CHE 303 Introduction to Chemical Engineering Thermodynamics Chapter 7 1 Thermodynamics of flow is based on mass, energy and entropy balances Fluid mechanics encompasses the above balances and conservation of momentum

More information

Applied Gas Dynamics Flow With Friction and Heat Transfer

Applied Gas Dynamics Flow With Friction and Heat Transfer Applied Gas Dynamics Flow With Friction and Heat Transfer Ethirajan Rathakrishnan Applied Gas Dynamics, John Wiley & Sons (Asia) Pte Ltd c 2010 Ethirajan Rathakrishnan 1 / 121 Introduction So far, we have

More information

Ulrich Walter. Astronautics. The Physics of Space Flight. 2nd, Enlarged and Improved Edition

Ulrich Walter. Astronautics. The Physics of Space Flight. 2nd, Enlarged and Improved Edition Ulrich Walter Astronautics The Physics of Space Flight 2nd, Enlarged and Improved Edition Preface to Second Edition Preface XVII Acknowledgments XIX List of Symbols XXI XV 1 Rocket Fundamentals 1 1.1 Rocket

More information

Theoretical and experimental study on heat transfer behaviour in gun tubes using aerosil additive for surface erosion protection

Theoretical and experimental study on heat transfer behaviour in gun tubes using aerosil additive for surface erosion protection Theoretical and experimental study on heat transfer behaviour in gun tubes using aerosil additive for surface erosion protection F. Seiler, H. Peter, G. Mathieu, G. Zettler French-German Research Institute

More information

Oin Figure 2. The peak gun launch pressure is 43,000 psi, which results in MAR

Oin Figure 2. The peak gun launch pressure is 43,000 psi, which results in MAR 'N GUN LAUNCH DYNAMICS OF THE NAVY S-INCH GUIDED PROJECTILE George Fotieo Martin Marietta Aerospace Orlando, Florida ABSTRACT,The design and qualification of the Navy 5-inch guided projectile components

More information

U S ARMY MISSILE COMMAND

U S ARMY MISSILE COMMAND REPORT NO. RF-TR-63..7 COPY NO. 8 143 311 t--... PARAMETRIC DESIGN CURVES FOR SHORT RANGE, r L "HIGH ACCELERATION BALLISTIC ROCKETS c C-- I April 1963 U S ARMY MISSILE COMMAND REDSTONE ARSENAL, ALABAMA

More information

Structural Integrity Analysis of Propellant in Solid Rocket Motor

Structural Integrity Analysis of Propellant in Solid Rocket Motor Structural Integrity Analysis of Propellant in Solid Rocket Motor Tejas Nikam 1, Mrunal Pardeshi 2, Amit Patil 3, Akshay Patkure 4, Manoday Ramteke 5 1 UG Student, Mechanical Engineering Department, Smt.

More information

^55. r? OB -/> Date. APPROVED: 7\ / LJCtJt^^^^ SAULT COLLEGE OF APPLIED ARTS & TECHNOLOGY SAULT STE, MARIE, ONTARIO COURSE OUTLINE

^55. r? OB -/> Date. APPROVED: 7\ / LJCtJt^^^^ SAULT COLLEGE OF APPLIED ARTS & TECHNOLOGY SAULT STE, MARIE, ONTARIO COURSE OUTLINE ^55 SAULT COLLEGE OF APPLIED ARTS & TECHNOLOGY SAULT STE, MARIE, ONTARIO COURSE OUTLINE Course Title: Code No -: Program: APPLIED THERMODYNAMICS MCH 206 MECHANICAL TECHNOLOGY Semester Date Author JUNE

More information

Study of Internal & External Ballistics for.177 cal &.22 cal Projectiles Ibraheem Raza Khan BE Student Department of Mechanical Engineering

Study of Internal & External Ballistics for.177 cal &.22 cal Projectiles Ibraheem Raza Khan BE Student Department of Mechanical Engineering IJSRD - International Journal for Scientific Research & Development Vol. 5, Issue 07, 2017 ISSN (online): 2321-0613 Ibraheem Raza Khan BE Student Department of Mechanical Engineering Abstract This is a

More information

ANALYSIS OF THE EFFECT OF PROPELLANT TEMPERATURE ON INTERIOR BALLISTICS PROBLEM

ANALYSIS OF THE EFFECT OF PROPELLANT TEMPERATURE ON INTERIOR BALLISTICS PROBLEM Journal of Thermal Engineering, Vol. 4, No. 4, Special Issue 8, pp. 2127-2136, Yildiz Technical University Press, Istanbul, Turkey ANALYSIS OF THE EFFECT OF PROPELLANT TEMPERATURE ON INTERIOR BALLISTICS

More information

COMBUSTION OF FUEL 12:57:42

COMBUSTION OF FUEL 12:57:42 COMBUSTION OF FUEL The burning of fuel in presence of air is known as combustion. It is a chemical reaction taking place between fuel and oxygen at temperature above ignition temperature. Heat is released

More information

Galactic Spacecraft. First Edition Tuesday, July 10, Maxim Thibodeau

Galactic Spacecraft. First Edition Tuesday, July 10, Maxim Thibodeau First Edition Tuesday, July 10, 2018 Maxim Thibodeau INDEX STANDARD LIMITATION...3 THE ETHEREAL EA PROPULSION...5 THE EA VERSION I... 6 THE SELF GAZ SEPARATOR...7 BOTH TWO WAYS... 8 EXOTHERMIC TYPE...

More information