Nan Yang
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To be more accurate, EADS Astrium is the main contractor, manager and launcher. iSRO is responsible for a small out sourced portion of building the two satellites. Hardly qualified as saying India is selling any of their satellite.
To be more accurate, "your" semi cryogenic is designed by Ukraine and the parts fabricated in India. Ukraine has full rights. You cannot change the design without their approval.So since journos are not informed such a project do not exist ? I have never seen anyone relying more on some news agency than an official source,an article written by none other Deputy Director of Cryogenic Propulsion in ISRO's Liquid Propulsion Systems Centre,who is also the chief designer of ISRO's CE 20 engine.
Mr. Kiran Kumar told The Hindu, “[The MoU] is the initial process, a lot of discussions must be held before it takes a concrete shape. We would work on future systems of common interest. We have identified several areas and established working groups to go through them. We have to see how it develops.”
The ISRO is working on its new-generation, Rs. 1,800-crore third rocket programme, called the semi-cryogenic launch vehicle, to beef up its current portfolio of the PSLV and the GSLV. It will use space-grade kerosene and liquid oxygen as fuel and is meant to pitch spacecraft totally weighing six to ten tonnes to heights of 36,000 km. This would be double the lifting power of the GSLV and triple that of the PSLV. Only the U.S. and Russia have this technology.
Mr. Kiran Kumar said: “We are looking at using Russian testing facilities for the semi-cryogenic engine. We will be ready with the engine [SCE-200] in six to eight months. Although we will have our own test facility at Mahendragiri, ours will take some time to come up.”
Russian tie-up to boost ISRO’s semicryogenic launcher plan - The Hindu
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ISRO plans launch schedules only two years in advance.Even according to the most pessimistic estimates,you'll see an ULV launch before 2020,for sure since it is a modification of the existing LVM 3 design with the semi cryogenic stage ( SC 160 ) replacing the existing hypergolic fueled one (L-110).About the semi cryogenic engine...
Published : July 11, 2015
Mr. Kiran Kumar said: “We are looking at using Russian testing facilities for the semi-cryogenic engine. We will be ready with the engine [SCE-200] in six to eight months. Although we will have our own test facility at Mahendragiri, ours will take some time to come up.”
The HLV would use the same engines as you as ULV.
ISRO is designing heavy-lift launch vehicles with capabilities in the range of 6–10 tonnes in GTO. For this purpose, the following propulsion systems are being pursued:
1. A 200 tonne propellant loading LOX and kerosene booster stage powered by a 2,000 kN
thrust semi-cryogenic engine operating on stage combustion cycle.
2. A 50 tonne LOX-LH2 propellant loading cryogenic stage powered by twin CE 20 cryogenic
engines.
3. A 10 tonne LOX-LH2 propellant loading cryogenic stage powered by a CE 20 cryogenic
engine.
This is not a measuring contest.
Any more dumb comments ?