Development on the Starburst began in the mid-1980s to meet a requirement by the British
Ministry of Defense. The missile was a development of the
Javelin missile, retaining the Javelin missile body but replacing the
radio command system with a
beam-riding guidance similar to that used by the
Starstreak missile that was already under development. This is much more difficult to
jam than the radio-based system used by Javelin. The targeting system itself was developed by
Thomson-CSF (now also a part of Thales Air Defense). The first shoulder-launched test firing took place in 1986 and development was completed in 1989. The base form of the Starburst consists of two components– the missile in its launching tube and the clip-on targeting system. The missile itself has a two-
stage motor that can be configured to detonate by
proximity or on
contact. The firing tube needs to be discarded after use, but the targeting system (developed by French electronics corporation Thomson-CSF) is reusable. == Combat history ==