Polar Satellite Launching Vehicle
The Pslv or polar satellite launching vehicle is a medium class launching vehicle. It is designed to launch satellite to sun-synchronus orbit. It is designed and Operated by ISRO Indian Space Research Organization. It is the third launching vehicle of ISRO after Augment Satellite Launching vehicle (ASLV).
PSLV profile
Function - medium lift launch vehicle
Booster's
No of booster (XL) - 6
No of booster (QL) - 4
No of booster (DL) - 2
Lendth - 12 m
Diameter - 1m
mass - 12,600 kg
Thrust - 703.5 km
Burn time - 70 second
Fuel - HTPB
First stage
Length - 20 m(66 ft)
Diameter - 2.8 m(9.8 ft)
mass - 138,200 kg
Thrust -
Burn time - 110 second
Fuel - HTPB
Second stage
Length - 12.8 m
Diameter - 2.8 m
mass - 42,000 kg
Engine - 1 Vikas
Thrust - 803.7 km
Burn time - 133 second
Fuel - N2 O4/UDMH
Third stage
Length - 3.6 m
Diameter - 2 m
mass - 7,600 kg
Thrust - 240 kn
Burn time - 83 second
Fuel - HTPB
Fourth stage
Length - 3 m
Diameter - 1.3 m
mass - 2,500 kg
Engine - 2 x L - 2 - 5
Thrust - 14.66 kn
Burn time - 425 second
Fuel - MMH/MON
Pslv c 34 sitting in launch pad |
PSLV profile
Function - medium lift launch vehicle
Country of origin - 🇮🇳 India
Cost per launch - $21-31 million
Height - 44 m
Diameter - 2.8 m
Stages - 4
Capacity
Payload to LEO - 3,800 kg
Payload to SSO - 1,750 kg
payload to sub-GTO - 1,425 kg
Payload to GTO - 1,200 kg
First launch
PSLV G - 20 September 1993
PSLV Ca - 23 April 2007
PSLV XL - 22 October 2008
PSLV QL - 1 April 2019
PSLV G booster's
No.of booster's - 6
Burn time - 44 second
Fuel - HTPB
Cost per launch - $21-31 million
Height - 44 m
Diameter - 2.8 m
Stages - 4
Capacity
Payload to LEO - 3,800 kg
Payload to SSO - 1,750 kg
payload to sub-GTO - 1,425 kg
Payload to GTO - 1,200 kg
First launch
PSLV G - 20 September 1993
PSLV Ca - 23 April 2007
PSLV XL - 22 October 2008
PSLV QL - 1 April 2019
PSLV G booster's
No.of booster's - 6
Burn time - 44 second
Fuel - HTPB
Booster's
No of booster (XL) - 6
No of booster (QL) - 4
No of booster (DL) - 2
Lendth - 12 m
Diameter - 1m
mass - 12,600 kg
Thrust - 703.5 km
Burn time - 70 second
Fuel - HTPB
First stage
Length - 20 m(66 ft)
Diameter - 2.8 m(9.8 ft)
mass - 138,200 kg
Thrust -
Burn time - 110 second
Fuel - HTPB
Second stage
Length - 12.8 m
Diameter - 2.8 m
mass - 42,000 kg
Engine - 1 Vikas
Thrust - 803.7 km
Burn time - 133 second
Fuel - N2 O4/UDMH
Third stage
Length - 3.6 m
Diameter - 2 m
mass - 7,600 kg
Thrust - 240 kn
Burn time - 83 second
Fuel - HTPB
Fourth stage
Length - 3 m
Diameter - 1.3 m
mass - 2,500 kg
Engine - 2 x L - 2 - 5
Thrust - 14.66 kn
Burn time - 425 second
Fuel - MMH/MON
Comments
Post a Comment