An experimental investigation of the starting and operational characteristi
cs of a 38-mm bore ram accelerator with propellant till pressures greater t
han 5 MPa is in progress. Successful starts with 60 - 124 gm projectiles ha
ve been achieved using methane/oxygen/niuogen propellants at fill pressures
ranging from 6 to 15 MPa. At fill pressures of 8.5 MPa and above, it was f
ound that projectiles having the nominal throat diameter (29 mm) required a
minimum entrance velocity of 1250 m/s, which is about 100 m/s faster than
the minimum needed to successfully start the ram accelerator at fill pressu
res below 7.5 MPa. Projectiles with a reduced throat diameter (25 mm) and a
solid magnesium nose cone were successfully started at 611 pressures up to
15 MPa with entrance velocities around 1300 m/s. The average accelerations
achieved using high pressure stages were in general less than predicted fo
r thermally choked operation by the Boltzmann equation of state.