An experimental investigation has been undertaken to improve understanding
of the role of the obturator and detonations in the subdetonative ram accel
erator starting process. Ram accelerator start experiments were conducted w
ith various obturator geometries to determine the obturator dynamics and as
sess its effect on the outcome of a start attempt. The obturator rapidly de
celerates upon entrance and then moves backwards. Reversal of direction occ
urs more rapidly after propellant ignition, for less massive obturators, an
d solid geometries. Perforated geometries and decreasing obturator mass are
less conducive to igniting a given propellant, as evidenced by the flowfie
ld and start attempt outcome data presented. Wave unstarts were observed to
occur with and without detonations, indicating more than one mechanism res
ponsible for this type of start failure. Piston-initiated detonation experi
ments were conducted by firing the obturators without the ram accelerator p
rojectile. The piston experiments identified the detonation limits for a wi
de range of propellants, but were found to not always be indicative of the
upper Mach number at which a ram accelerator can be successfully started. I
n some instances a successful start or wave fall-off would occur at Mach nu
mbers above which a piston alone detonated the propellant. Thus, the projec
tile can play a mitigating role in detonation initiation and use of piston
detonation limits to quantitatively define a detonation wave unstart limit
was not realized.