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Separation and Staging Mechanisms for the Indian SLV-3 Launch VehicleA unique separation and jettison system for the ascent fairing and a staging system for the apogee motor of the first Indian satellite launch vehicle are described. Design features, development problems, and mission constraints are discussed in addition to the solutions adopted. A qualification summary is included for each system, and flight results obtained from SLV-3 launches are described.
Document ID
19840017027
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abdulmajeed, M. K.
(Indian Space Research Organization Trivandrum., United States)
Matarajan, K.
(Indian Space Research Organization Trivandrum., United States)
Krishnankutty, V. K.
(Indian Space Research Organization Trivandrum., United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1984
Publication Information
Publication: NASA. Goddard Space Flight Center The 18th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
84N25095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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