SIDDA.MANIKANTA
13761A2134
AEROSPACE Engg.
LBRCE {AP}
PRESENTATION BY:
PRESENTATION BY :
SIDDA.MANIKANTA
13761A2134
AEROSPACE Engg.
LBRCE {AP}
 “ SPACE SHUTTLE ” Officially known as
“ Space Transportation System ” {STS} .
 In 1969 a thought of Reusable Spacecraft was raised
and as a result Space Shuttle was in operation.
 In that plan it was the only item to be funded.
 Finally it was tested in 1981 and these were
operational from 1982.
 During their period of operation from 1981-2011
they were used in 135 missions.
 Space shuttle
components includes
1) External tank
2) Pair of SRBs
3) Orbiter vehicle
 EXTERNAL TANK :-
 Its function is to supply liquid oxygen and hydrogen to
Main engines . It acts as backbone to vehicle providing
Attachments to SRBs and orbiter .
 PAIR OF SRBs :-
 Solid rocket boosters function is to provide initial thrust
during liftoff that is about 85%.they were jettisoned two
minutes after launch.
 ORBITER VEHICLE :-
 Its function is to introduce payload into the earth orbit.
COLLECTING OF EXTERNALTANK & SRBs
ROBOTIC ARM OF SPACE SHUTTLE
SPACE SHUTTLE DURING RE-ENTRY
THERMAL PROTECTION SYSTEM:-
 TPS on the orbiter is the biggest defense system
to the heat encountered during re-entry.
 TPS mainly constitutes of tiles , which are reusable.
 Tiles are made up of “ Amorphous silica fiber ” and
these are able to withstand 3000 F.
REUSABLE CERAMIC TILES:-
COMPOSITION OF TILES
 These tiles consists of
90% air and remaining
10% silica fiber.
 As these are bad
conductors of heat they
can touch with bare
hands at 2200F.
Tiles at 2200F taken from a woven.
TESTING OF TILES;-
SPACE SHUTTLE
SPACE SHUTTLE
SPACE SHUTTLE

SPACE SHUTTLE