cabatli_53
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Sorry but Who prepared such wrong sheet to make favour of WZ-10 ?
How logical is it ?
-2*1014kw proven motor of Atak carry 5000kg fuselage to 6096m altitude but, 2*1000kw motor make 7000kg WZ-10 to climb 6400m ? How possibile is it ?
-T-129 Atak with more powerfull power/weight ratio than WZ-10, have a rate of climb 14m/s but WZ-10 is 15+m/s ? How possible ?
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