The design, construction, and the testbed results for a novel compact
gas gun injector for solid diagnostic pellets of different sizes and m
aterials is reported here. The injector was optimized for the diagnost
ic requirements of the ASDEX Upgrade tokamak, yielding the possibility
of a widely varying deposition profile of ablated material inside the
plasma. This allows variation of the pellet velocity and the total nu
mber of injected atoms. The use of spherical carbon pellets and differ
ent propellant gases (He,N2,H-2) results in an accessible velocity ran
ge from about 150 m/s to more than 600 m/s and pellet masses from 2 x
10(18) to 10(20) atoms. Both the scattering angle (approximately 1-deg
rees) and the maximum propellant gas throughput to the tokamak (less t
han 10(16) gas particles) were found to be sufficiently low. The injec
tor provided both high efficiency (greater-than-or-equal-to 85%) and h
igh reliability during the whole testbed operation period and also dur
ing the first injection experiments performed on ASDEX Upgrade. The pe
llet velocities achieved for different propellant gas pressures and pe
llet diameters were analyzed. It was discovered that, although the pel
let diameters range from 0.45 to 0.85 times the barrel diameter, the p
ellet acceleration is mostly caused by gas drag. Pellet velocities in
excess of those calculated on the basis of the gas drag model were obs
erved. Additional acceleration that increases with the pellet diameter
contrary to the gas drag model may be explained by the influence of t
he pellet on the gas dynamics in the barrel.