There is an amateur rocket group in Australia called Ausroc. In 1989
they launched their first rocket, a liquid fueled rocket based upon
a modified Pacific Rocket Society design. This rocket, called Ausroc I 
was launched on 9 Feb. 1989 from the army proving ground at Puckapunyal.
The flight lasted one minute, reaching 3 km in altitude and 161 m/s.

The group is now preparing to launch an all Australian rocket from 
Woomera (which has previously put 2 satellites into orbit). Ausroc
is also working on a third liquid fueled rocket called Ausroc III.

The specifications for Ausroc II are:

Length		   5600 mm	Propellant mass	         89 kg
Diameter	    258 mm	Fueled mass             219 kg
Fin tip distance    858 mm	Mass ratio             0.41
Fin length	    500 mm      Sensors	  2 accelerometers
Fin width	    300 mm		  3 pressure transducer
Nose length	    500 mm		  1 temperature transducer
Thrust		   9810 N	          1 CCD monochrome video camera   
Burn time	     20 s	Transmitter frequency   444 MHz
Specific impulse   2305 m/s     Transmitter power	 10 W
Fuel	       kerosene 	Electronics	8051 microprocessor
Fuel mass	     30 kg			8 channel input/output
Fuel volume	     38 l			10 bit A/D converter
Oxidiser	    LOX		Memory		1 Mbyte EPROM
Oxidiser mass	     59 kg	Power supply	2 dry lithium battery packs
Oxidiser volume	     16 l       Launch guide rail        10 m
Pressurisation gas   Helium	Launch angle		 70 degrees
Tank pressure	     20 MPa     Expected apogee	       11.3 km
Gas bottle volume    16 l	Expected range	       25.5 km
Dry mass	    130 kg