This report covers the 'B' series launcher release tests. Two simulated missile launches of 10 inches free travel were made at a thrust/weight (T/W) ratio of 1.33 and two simulated missile launches of 11 inches free travel were made at a thrust/weight (T/W) ratio of 1.48. These tests were also used as the dynamic check-out for the 'B' series release curves. (Author)


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    Atlas/Centaur launcher tests

    Eastwood, C. W., Jr. / Humphrey, J. | NTRS | 1967


    Lance Missile Launcher Stability Tests

    G. W. Leese / J. L. Decell | NTIS | 1967




    Launcher Hold and Release Mechanism for GSLV

    Purushothaman, P. | British Library Online Contents | 1997