Exploratory development of the reconnection launcher 1986-90

Abstract

The exploratory development phase for the reconnection launcher is summarized. This is an induction launcher which features a contactless, solid armature with either flat-plate or cylindrical geometry. The strategy for successful design is discussed, emphasizing the way the issues of ohmic heating and high-voltage requirements for high velocity were resolved. The indispensable role of a fast-running, mesh-matrix code is stressed. The three multistage launcher are described. One of these achieved a muzzle velocity of 1 km/s with a 150 gram flat-plate projectile. The other two have launched cylindrical projectiles at 335 m/s, one with relatively heavy projectiles of 5 kg, the other with relatively light ones of 10 g. The cylindrical projectile scan be spin-stabilized prior to launch for improved flight. The potential of this technology for earth-to-orbit launch of small artificial satellites is outlined.< <ETX xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">&gt;</ETX>