CHANDRAYAAN
- 2
ISRO- INDIAN SPACE RESEARCH ORGANISATION
LAUNCHED FROM 2ND
LAUNCH PAD OF
SATISH DHAWAN
SPACE CENTRE ,
SRIHARIKOTA.
GSLV MARK III
CONSISTS OF THREE
PAYLOADS:
1.LUNAR ORBITER
2.VIKRAM LANDER
3.PRAGYAN ROVER
>>THE CRAFT REACHED THE MOON’S
ORBIT ON 20 TH AUGUST 2019 AND
BEGAN ORBITAL POSTIONING FOR
LANDING OF VIKRAM LANDER……
OBJECTIVES AND DESIGN OF GSLV MARK III :
TO DEMONSTRATE THE ABILITY TO SOFT LANDING ON THE LUNAR
SURFACE OF SOUTH POLE REGION AND OPERATE A ROBOTIC ROVER
ON IT…..
SCIENTIFIC GOALS INCLUDE ORBITAL STUDIES OF :
>>LUNAR TOPOGRAPHY
>>MINERALOGY
>>ELEMENTAL ABUNDANCE
>>WATER ICE
>> WATER ON LUNAR SURFACE
3
LUNAR ORBITER :
4
>>Weight : 2379 kg
>>Power : 1000 watts
>>It consists of 8 payloads
>>capable of communicating
with ” INDIAN DEEP SPACE
NETWORK “ (IDSN) at
Bayalalu as well as the
vikram Lander ……
VIKRAM LANDER :
Weight : 1471 kg
Power : 650 watts
>>The lander of chandrayan -2 was
named VIKRAM after
Dr.Vikram A Sarabhai the father of
the Indian space Programme.
>>It was designed to funtion for
one lunar day which is equivalent
to 14 Earth days.
>> It consists of four payloads.
5
PRAGYAN ROVER :
>>Chandrayaan- 2 Rover
was a six wheeled robotic
vehicle named as Pragyan.
>>Which translates to
“wisdom” in Sanskrit.
Weight : 27 kg
Power : 50 watts
>>It consists of
two payloads.
6
TRAVELLING AND REACHING POSITION:
LANDING POSITION ::
>>Vikram was designed
to perform soft land in
the south polar region.
of the moon between
two craters ,Manzinus C
and Simpelius N on
September 7 th.
However the lander deviated
from its intended trajectory at
2.1 km altitude and had lost
communication when touch
down confirmation was
expexted .
>>ISRO chairman Dr. K.Sivan
stated that it must be hard
landing…….
7
DISCONNECTION
PROCESS:
>>ISRO AND NASATRIEDTO
RECONNECT IT BUT WE WERE
UNABLETO RECONNECT IT.
WWW.CHANDRAYAN 2
9
10
PROUD TO
BE AN
INDIAN…….

Chandrayaan-2

  • 1.
    CHANDRAYAAN - 2 ISRO- INDIANSPACE RESEARCH ORGANISATION
  • 2.
    LAUNCHED FROM 2ND LAUNCHPAD OF SATISH DHAWAN SPACE CENTRE , SRIHARIKOTA. GSLV MARK III CONSISTS OF THREE PAYLOADS: 1.LUNAR ORBITER 2.VIKRAM LANDER 3.PRAGYAN ROVER >>THE CRAFT REACHED THE MOON’S ORBIT ON 20 TH AUGUST 2019 AND BEGAN ORBITAL POSTIONING FOR LANDING OF VIKRAM LANDER……
  • 3.
    OBJECTIVES AND DESIGNOF GSLV MARK III : TO DEMONSTRATE THE ABILITY TO SOFT LANDING ON THE LUNAR SURFACE OF SOUTH POLE REGION AND OPERATE A ROBOTIC ROVER ON IT….. SCIENTIFIC GOALS INCLUDE ORBITAL STUDIES OF : >>LUNAR TOPOGRAPHY >>MINERALOGY >>ELEMENTAL ABUNDANCE >>WATER ICE >> WATER ON LUNAR SURFACE 3
  • 4.
    LUNAR ORBITER : 4 >>Weight: 2379 kg >>Power : 1000 watts >>It consists of 8 payloads >>capable of communicating with ” INDIAN DEEP SPACE NETWORK “ (IDSN) at Bayalalu as well as the vikram Lander ……
  • 5.
    VIKRAM LANDER : Weight: 1471 kg Power : 650 watts >>The lander of chandrayan -2 was named VIKRAM after Dr.Vikram A Sarabhai the father of the Indian space Programme. >>It was designed to funtion for one lunar day which is equivalent to 14 Earth days. >> It consists of four payloads. 5
  • 6.
    PRAGYAN ROVER : >>Chandrayaan-2 Rover was a six wheeled robotic vehicle named as Pragyan. >>Which translates to “wisdom” in Sanskrit. Weight : 27 kg Power : 50 watts >>It consists of two payloads. 6
  • 7.
    TRAVELLING AND REACHINGPOSITION: LANDING POSITION :: >>Vikram was designed to perform soft land in the south polar region. of the moon between two craters ,Manzinus C and Simpelius N on September 7 th. However the lander deviated from its intended trajectory at 2.1 km altitude and had lost communication when touch down confirmation was expexted . >>ISRO chairman Dr. K.Sivan stated that it must be hard landing……. 7 DISCONNECTION PROCESS:
  • 8.
    >>ISRO AND NASATRIEDTO RECONNECTIT BUT WE WERE UNABLETO RECONNECT IT. WWW.CHANDRAYAN 2
  • 9.
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