The document outlines India's space vision for 2025, which includes developing satellite-based rural connectivity systems, enhanced imaging for resource management, space science missions, and planetary exploration. It describes India's existing launch vehicle family and capabilities for Mars, Venus, and asteroid missions. The vision also involves developing a heavy lift launcher, reusable launch vehicles, and human space flight missions using GSLV MkIII and a crew module. The goal is to develop advanced propulsion technologies like air-breathing and cryogenic engines to enable interplanetary missions and ultimately lower-cost single-stage-to-orbit vehicles.

1. SPACE VISION INDIA : 2025
Presented by :-

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

3. MAJOR POINTS
• 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

4. In the year : 2025

5. Reusable Launch Vehicle
… for repeated use of the costly
hardware

6. Reusable Launch Vehicle using Air Breathing Propulsion

7. ISRO Launch Vehicle Family
Aug 1979 /July 1980 May 1992 Oct 1994 Apr 2001 Middle 2010
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

8. Missions to Mars, Venus,
Asteroids
Flyby Capabilities (kg) Orbital Capabilities (kg)
Mars Venus Asteroid Mars Venus Asteroid
728-777 717-766 556-862 PSLV 172-213 107-146 80-186
1219-1302 1260-1346 625-1514 GSLV 402-584 247-328 150-443
2617-2793 2705-2890 1342-3250 Mk III 882-1060 542-719 182-972

9. CHANDRAYAAN-1 CHANDRAYAAN-2

10. Chandrayaan 1
 Launched by PSLV 11: 313 t
 Date of Launch : 22nd Oct 2008
Chandrayaan 1
India 1380 kg

11. Labeled figure of CHANDRAYAAN-2

12. Indian Human Space Flight Programme
To develop a space vehicle to carry crew of two to LEO and return safely to a
predetermined destination on earth
Crew escape system (ces)
Crew module
Service module
Orbital vehicle

13. Human Space Mission : Vehicle configuration
GSLV MkII Manned Configuration Manned capsule
Launch
Escape
System
Vehicle Height : 51.5 m
Lift-off Mass : 417 t Crew Module
Service Module

14. Indian Space Transportation Vision 2025
Indigenous Cryogenic Upper Stage (CUS) 2009
Geo Synchronous Launch Vehicle MK III
2010
Semi cryogenic Engines
2015
Indian Human Space Mission
Reusable Launch Vehicle 2016
High thrust cryogenic Engine Boosters
2017
Air- breathing Engines
2018 Interplanetary Mission to beyond MARS
Advanced Propulsion for Planetary Exploration
2020 Two Stage To Orbit to reduce the Cost
Single Stage To Orbit using Air breathing Propulsion
2025

15. Thank You