I do not agree with you as the thrust parameters as stated by you have yet to be achieved. When I calculated the TWR of Kaveri upgraded by SAFRAN, i used the current weight of Kaveri which is about 1125kgs. The refined Kaveri may turn out to be 1050 kgs design as it is just 3.5m long plus new materials in some of the core areas will result in that kind of weight saving. If the weight comes down to 1050kgs, the TWR will be over 11:1.
The thrust parameters for all the above engines have been met, minus the Type 30. They are all in serial production in some form or the other.