this ppt is about ISRO's recent successful launch Geostationary Launch Vehicle

2. Contents
Introduction
Features
Stages
Profile
CARE
Future
Conclusion
References

4. Features of GSLV Mark-III
 Biggest launch vehicle so far.
 By this ISRO’s human spaceflight
programme aims to send two astronauts into
LEO and bring them back safely.
 It is also significant from the perspective of
ISRO’s own cryogenic engine.

6. Stage-1: Solid Boosters
 These boosters burn for 130sec and
produce a peak thrust of about 5150 kilo
newton each.
 It has a large nozzle which helps in
orientation.

7. Stage 2: Liquid motor
 The core stage designated L110, produce
700 Kilo newton uses regenerative cooling.
 The core stage designated is a 4 meter
diameter carrying 110 tonnes of UDMH and
N2O4.
 It is the first Indian liquid-engine cluster
design and uses two improved Vikas engines.

8. Stage 3: Cryogenic stage
 It is designated as C25, will be
powered by the Indian developed CE-20
engine burning LOX and LH2 producing
186 kilo newtons.

11. CARE separated from the passive C25 cryogenic upper
stage of GSLV Mk-III 330.8 seconds after lift-off and
began its guided descent for atmospheric re-entry.

12. After the successful re-entry phase, CARE
module’s parachutes opened, following which it
gently landed over Andaman Sea about 1600 km
from Sriharikota.

13. The first orbital flight is planned
to take place in 2016.
The first flight with a crew on
board would take place after 2020

14.  The successful launch of ISRO’s
GSLV MARK-III make India fully self
dependent in launching heavier
communication satellites of INSAT-4
class, which weigh 4500-5000Kg.

16. References
http://antariksh-space.blogspot.in/2013/01/isro-
reusable-launch-vehicle-program.html
http://spaceflightnow.com/2014/12/17/powerful-new-
indian-rocket-poised-for-suborbital-test-launch/
http://www.pragyan.org/blog/2014/12/another-leap-
into-space/
http://en.wikipedia.org/wiki/Geosynchronous_Satellite
_Launch_Vehicle_Mk_III