An overview of the applications of holographic interferometry for spac
ecraft structural components at ISRO Satellite Centre, Bangalore, Indi
a, is presented. The details of the development of a dual vacuum stres
sing technique and its application for holographic nondestructive test
ing (HNDT) of honeycomb panels are presented. Results of some calibrat
ion studies conducted for HNDT of propellant tanks are also presented.
It is found that holographic interferometry is quite useful, particul
arly for HNDT of honeycomb panels and propellant tanks used for spacec
raft structural components.