Hi guys, ISRO is all set to test a loads of new technologies improve the performance of its launch vehicles which includes and low weight parts, Air breathing technology, scram jet etc. I am starting this new thread to discuss the implications of these technologies on India's missile program. Once we start using All composite missile with high efficiency NEPE like fuel with low weight components and motors with Air breathing and scram jet technology than we may bring manifold efficiency in our missile technology. Can we use that duel pulse technology in our big motors? Once we incorporate all these new technology than what is the degree of efficiency can we achieve in our missiles? Let us discuss.