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Exploratory development of the reconnection launcher, 1986--1990

Conference ·
OSTI ID:7251071
We briefly summarize the exploratory development phase for the reconnection launcher. 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 we resolve the issues of ohmic heating and high-voltage requirements for high velocity. The indispensable role of a fast-running, mesh-matrix code is stressed. We describe three multistage launchers. One of these achieved 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 grams. The cylindrical projectiles can be spin-stabilized prior to launch for improved flight. We outline the potential of this technology for earth-to-orbit launch of small satellites. 19 refs., 9 figs.
Research Organization:
Sandia National Labs., Albuquerque, NM (USA)
Sponsoring Organization:
DOE/DP
DOE Contract Number:
AC04-76DP00789
OSTI ID:
7251071
Report Number(s):
SAND-90-0630; CONF-9004136--7; ON: DE90008578
Country of Publication:
United States
Language:
English

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