JNTU 2007-2008 III YEAR II SEM. B. TECH. AE - INTRODUCTION TO SPACE TECHNOLOGY

Posted Date: 09 Dec 2007 Resource Type: Articles/Knowledge Sharing Category: Syllabus

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JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY
HYDERABAD
III Year B. Tech. AE – II semester T P C
4+1* 0 4
INTRODUCTION TO SPACE TECHNOLOGY

UNIT-I
INTRODUCTION
Space Mission-Types-Space Environment-Launch Vehicle Selection

UNIT II
FUNDAMENTALS OF ROCKET PROPULSION
Introduction to rocket propulsion-fundamentals of solid propellant rockets- Fundamentals of liquid propellant rockets-Rocket equation

UNIT-III
ASCENT FLIGHT MECHANICS OF ROCKETS AND MISSILES
Two-dimensional trajectories of rockets and missiles-Multi-stage rockets-Vehicle sizing-Two stage Multi-stage Rockets-Trade-off Ratios-Single Stage to Orbit- Sounding Rocket-Aerospace Plane-Gravity Turn Trajectories-Impact point calculation-Injection conditions-Flight dispersions

UNIT-IV
ATMOSPHERIC REENTRY
Introduction-Steep Ballistic Reentry-Ballistic Orbital Reentry-Skip Reentry-“Double-
Dip” Reentry - Aero-braking - Lifting Body Reentry
UNIT-V
FUNDAMENTALS OF ORBITAL MECHANICS
Two-body motion-Circular, elliptic, hyperbolic, and parabolic orbits-Basic Orbital
Elements-Ground Trace
UNIT-VI
ORBITAL MANEUVERS
In-Plane Orbit changes-Hohmann Transfer-Bielliptical Transfer-Plane Changes- Combined Maneuvers-Propulsion for Maneuvers

UNIT -VII
SATELLITE ATTITUDE DYNAMICS
Torque free Axi-symmetric rigid body-Attitude Control for Spinning Spacecraft - Attitude Control for Non-spinning Spacecraft - The Yo-Yo Mechanism – Gravity – Gradient Satellite-Dual Spin Spacecraft-Attitude Determination

UNIT-VIII
SPACECRAFT POWER AND COMMUNICATION SYSTEMS
Spacecraft Power-Telecommunications

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