ISRO Rocket complete information
ISRO Rocket complete information
THE FIST ISRO ROCKET
What is SLV 3 ROCKER
Satellite Launch Vehicle-3 (SLV-3) was India's first experimental satellite launch vehicle, which was an all solid, four stage vehicle weighing 17 tonnes with a height of 22m and capable of placing 40 kg class payloads in Low Earth Orbit (LEO).
SECOND ISRO ROCKET
What is ASLV ROCKET
With a lift off weight of 40 tonnes, the 24 m tall ASLV was configured as a five stage, all-solid propellant vehicle, with a mission of orbiting 150 kg class satellites into 400 km circular orbits.
THREAD ISRO ROCKET
What is PSLV ROCKET
Polar Satellite Launch Vehicle (PSLV) is the third generation launch vehicle of India. It is the first Indian launch vehicle to be equipped with liquid stages.
The vehicle successfully launched two spacecraft – Chandrayaan-1 in 2008 and Mars Orbiter Spacecraft in 2013 – that later traveled to Moon and Mars respectively.
Vehicle Specifications
Height : 44 m
Diameter : 2.8 m
Number of Stages : 4
Lift Off Mass : 320 tonnes (XL)
Variants : 3 (PSLV-G, PSLV - CA, PSLV - XL)
First Flight : September 20, 1993
FORT ISRO ROCKET
What is GSLV ROCKET
ISRO GSLV MK 3 complete information.
The third generation GSLV, inherits various technologies from its predecessors it's very different in terms of its stages,structure, size and has double the payload carrying capacity than the MK 2 version nearly 43.5 meter lall and with a lift-off mass of 641 tons.
Where Chandrayaan 2 was launched, the capacity of PSLV was 1 tonne+ to GTO spacecraft.
The GSLV MK 3 is a 4 metre-diameter class rocket,with a payload of 4 tonnes to GTO. this is the rocket that is going to carry our Chandrayaan 2 to the mid orbit.
The GSLV MK -3 is signified with a very very elegant architecture in which we use one of the biggest solid boosters called S200, as its strap-ons or the first stage.
Then we use a liquid stage, Vikas engine-based L110and a cryogenic upper stage a new cryogenic upper stage with C25 stage with CH20, 20-tonne thrust cryogenic engine. which is as indigenous development.
it also features a payload compartment which is 5 metres in diameter giving almost 100 metre payload volume.
Balancing of these 2 motors to provide very equal thrust in a solid motor was one of the importance, whallenges, which was addressed in the design and processing casting and testing of these motors.
S200 BOOSTERS
The first stage of this giant vehicle consists of the s200 boosters which are 26.2 meters long and 3.2 meters in diameter.
Each has a capacity of carrying 205 tons of solid propellant. S200 is the 3rd largest solid rocket motor in the world.
L110 core stage
The L110 core stage carried 116 torn of earth storable liquid propellants.
It is nearly 21.4 meter longs and 4 meter in diameter.
It employs two enhanced thrust Vikas engions.
C25 CRYOGENIC
The 13.5 meter long indigenous C25 CRYOGENIC Upper stage forms the third stage of the vehicle.
It uses 28.6 tons of supercooled Liquid Hydrogen and Liquid Oxygen which provides more thrust for every kilogram of propellant burn compared to conventional liquid propellants.
PAYLOAD FAIRING
On top of the third stage is the spacecraft
In the five-meter diameter payload fairing
The first successful experimental flight of GSLV MK3 took place in 2014 when it carried a crew module as its payload.
Both its solid and liquid propulsion stages had performed well and the vehicle was proven in the atmospheric flight regime.
The first developmental flight of GSLV MK 3 SUCCESSFULLY LAUNCHED India's high throughput communication satellite GSAT-19 weighing 3136 kilograms on 05th june 2017.
In the GSLV MK3 D2 mission.the rocket will carry the 3423 kilogram gate-29 communication satellite into Geosynchronous Transfer Orbit.
GSLV MK3 vehicle will lift-off watch the simultaneous ignition of its S200 boosters.
The ignition of the liquid core stage will be at 114 seconds into the flight.
Both the boosters will burnout and separate form the vehicle at 140 seconds after lift-off.
At 225 seconds, the payload fairing will separate.
At 317 seconds the liquid core stage will burn out and separate from the vehicle.
2 second later, the C 25 stage will ignite and will burn for almost 10 minutes
Subsequently it will shut dion at 965 seconds.
palode is planned to be injected into a gto with its perigee at 190 km and apogee at 36000 km.
GSLV Mk III Launches Till Date
SN Title Launch Date Payload
4 GSLV-Mk III - M1 Jul 22, 2019 Chandrayaan 2
3 GSLV Mk III-D2 Nov 14, 2018 GSAT-29
2 GSLV Mk III-D1 Jun 05, 2017 GSAT-19
1 LVM-3 Dec 18, 2014 Crew module Atmospheric Re-entry Experiment (CARE)
No comments:
Post a Comment