8 Interesting facts about GSLV MARK III
- GSLV MARK III
was successfully launched on June 5th of 2017. It was a prominent
step for the future programs of ISRO. It took 15 years to complete this project
with a budget of 300 core. - GSLV MARK 3
has one liquid and one solid propellant stage and a cryogenic stage. - GSLV MARK 3
has a capacity to launch a payload with 4000 kg
to a Geosynchronous Transfer Orbits of altitude
3600 km and It can place 8000 kg payload to low earth orbit of 600 km altitude. - This will
be an important step of ISRO towards their future plan to conduct a manned
space mission. The rocket has a weight of 640 ton and 43.43-meter height. - In the cryogenic
stage (Third stage) of GSLV MARK 3, liquefied
hydrogen is used as fuel and liquefied
oxygen as the oxidizer. Fuel and oxidizer
are stored in different tanks for space
vehicles because fuel alone can’t burn in space in the absence of oxygen. - The fuel-
oxygen mixture is burning in the combustion
chamber. The first stage is a solid propellant stage and the second one is a liquid
propellant stage. - ISRO tested
this GSLV MARK 3 in the Crew module Atmospheric Reentry Experiment(CARE) mission on December
18, 2014. - Currently, ISRO is using European Union’s ARIANE rocket to launch heavy satellites into orbit.GSLV Mark 3 will use from 2017.
Interesting facts about the three stages of GSLV MARK III
- The first
stage of the ignition is powered by the solid propellant
Hydroxyl-terminated polybutadiene(ITPB). - Two hundred
tons of propellant is burned for the ignition of the first stage engine “S200”. Simultaneously two booster
rockets of GSLV Mark 3 located on either side of its liquid booster will ignite
for 130 seconds.
- In the second
stage two Vikas Liquid Engine of L- 110 will work for 114 seconds after liftoff. The booster rockets will separate
after 140 seconds from lift-off. - The liquid propellant used here is 110 tons of mono
methane hydrosilane and nitrogen
triiodide. - The third
stage of GSLV Mark III is a cryogenic stage. Here liquid hydrogen and
oxygen are used as a propellant at a temperature of -252.87°C and
-182.82°C respectively. - The CE-20 engine used
in cryogenic stage and 25 tons of cryogenic fuel is burned during this stage.CE-20
is developed by the Liquid Propulsion Systems Centre.





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