Again, more loud mouth nonsense, but I'll indulge you:
http://www.nextbigfuture.com/2016/12/china-says-tests-of-propellentless.html
China says tests of Propellentless EMDrive on Tiangong 2 space station were successful
http://www.dailymail.co.uk/sciencet...-impossible-engine-says-s-orbiting-Earth.html
http://www.ibtimes.co.uk/emdrive-ch...al-tech-onto-satellites-soon-possible-1596328
But I'm sure the "SUPER-INNOVATIVE" Indians have been testing something x10 better on their SUPER INNOVATIVE (whilst frugal) ROBOTIC space station on the moon with robotic scientists.
Since you just seem so clueless on anything to do with space other that chest thumping "India stronk" nonsense(with 0 relevant sources), I'll post more links to CASC activities in the relevant thread.
YOU STILL HAVEN'T POSTED ANY LINK SO FAR ITS NOT ME ITS YOU WHO NEED TO BACK UP HOLLOW CHINESE PROGRAMME BASED ON STOLEN AND BOUGHT TECH NOT ME GET IT???
the electric propulsion you are talking about has been in only testing or proof of concept phase and nothing but HOT AIR FROM CHINA they CLAIMED it but nothing concrete so far give me some data instead of postinf tabloid articles show me a detailed document of the science that went it to and how it is different and what kind of thrust it generates beside we also field tested electric propulsion on our SATS long time ago
http://isro.org/gslv-d3/pdf/GSLV-D3_GSAT-4 Brochure.pdf
Presently LPSC, ISRO is actively engaged in the development of 75mN SPT to be used in its future high power communication satellites.
75 mN SPT
Thrust
Nominal mode : 75 mN ± 1 mN
Throttling mode : 50 ------ 100 mN
Mass of thruster : 8 kg ( Maximum)
Maximum thermal dissipation from thruster. : 260 Watt
250 mN SPT
Thrust
Nominal mode : 250 mN ± 15 mN
Throttling mode : 200 ------ 300 mN
Mass of thruster : 15 kg (Maximum)
Maximum thermal dissipation from thruster. : 450 watt
Source: http://www.isro.org/Tender/Lpsc-b/TENDER%20NOTICE%20NO-8-RFP.pdf
For comparison: DAWN's ION propulsion from wiki
1) The Dawn spacecraft is propelled by
three xenon ion thrusters
2) They have a specific impulse of 3,100 s and produce a thrust of
90 mN.
3) The whole spacecraft, including the ion propulsion thrusters, is powered by a 10 kW (at 1 AU) triple-junction gallium arsenide photovoltaic solar array
4) Dawn is allocated 275 kg (606 lb) of xenon, with another 110 kg (243 lb) to reach Ceres, out of a total capacity of 425 kg
(MOM is carrying 850 kg liquid propellant) of on-board propellant. With the propellant it carries, Dawn can perform a velocity change of more than 10 km/s over the course of its mission, far more than any previous spacecraft achieved with onboard propellant after separation from its launch rocket.
5) Dawn is NASA’s first purely exploratory mission to use ion propulsion engines.
ISRO is also funding development of yet another class of electric thruster called
Magnetoplasmadynamic Electric Propulsion Thruster
Magnetoplasmadynamic Electric Propulsion Thruster: Design, Fabrication and Application – ISRO Sponsored Project, IEPC 2013
this was way back in 2013 right now we have improved engine designs ready
and believe me when i say indian shuttle will revolutionize space propulsion and reduce costs to drastic level and generate huge profits from space launch ISRO GENERATED 100 MILLION FROM PROFITS LAUNCHING SATS ???
HOW MUCH DID THE SUPREME JUNK HAULER CHINA ACHIEVE?
the hall effect thrusters has long been used by ISRO and russia has been using for long too again nothing but hot air coming from you.