SPACE VISION INDIA : 2025

Presented by :-

CONTENTS• Introduction to major points• Description of the space vision: 2025• Types of launch vehicles• Missions to Mars, Venus, Asteroids• Human Space Missions• Summarization

• Satellite based communication systems for rural connectivity

• Enhanced imaging capability for natural resource management

• Space science missions• Planetary exploration • Development of Heavy lift launcher • Reusable Launch Vehicles - Technology demonstrator

missions leading to Two Stage To Orbit (TSTO) • Human Space Flight

MAJOR POINTS

In the year : 2025

Reusable Launch Vehicle

… for repeated use of the costly hardware

Reusable Launch Vehicle using Air Breathing Propulsion

ISRO Launch Vehicle Family

SLV ASLV PSLV GSLV

GSLV Mk-III

Height (m) 22 23.5 44 49 42.43

Lift-off wt(t) 17 39 295 414 632

Payload kg 40 150 1400 2000 4000

Orbit LEO LEO POLAR GTO GTO

Height (m) 22 23.5 44 49 42.43

Lift-off wt(t) 17 39 295 414 632

Payload kg 40 150 1400 2000 4000

Orbit LEO LEO POLAR GTO GTO

Aug 1979 /July 1980 May 1992 Oct 1994 Apr 2001 Middle 2010

Orbital Capabilities (kg)

Mars Venus Asteroid

PSLV 172-213 107-146 80-186

GSLV 402-584 247-328 150-443

Mk III 882-1060 542-719 182-972

Flyby Capabilities (kg)

Mars Venus Asteroid

728-777 717-766 556-862

1219-1302 1260-1346 625-1514

2617-2793 2705-2890 1342-3250

Missions to Mars, Venus, Asteroids

CHANDRAYAAN-1 CHANDRAYAAN-2

Chandrayaan 1 Launched by PSLV 11: 313 t

Date of Launch : 22nd Oct 2008

Chandrayaan 1India 1380 kg

Labeled figure of CHANDRAYAAN-2

Indian Human Space Flight ProgrammeTo develop a space vehicle to carry crew of two to LEO and return safely to a predetermined destination on earth

Orbital vehicle

Crew module

Service module

Crew escape system (ces)

GSLV MkII Manned Configuration

Launch

Escape

System

Crew Module

Service Module

Vehicle Height : 51.5 mLift-off Mass : 417 t

Manned capsule

Human Space Mission : Vehicle configuration

Semi cryogenic Engines

Indigenous Cryogenic Upper Stage (CUS)

Two Stage To Orbit to reduce the Cost

Geo Synchronous Launch Vehicle MK III

Indian Human Space Mission

High thrust cryogenic Engine Boosters

Interplanetary Mission to beyond MARS

Air- breathing Engines

Advanced Propulsion for Planetary Exploration

Single Stage To Orbit using Air breathing Propulsion2025

2009

2010

2015

Reusable Launch Vehicle 2016

2020

2018

Indian Space Transportation Vision 2025

2017

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