a5 (rocket)

The A5 was a German rocket with a length of 5.825 meters, a diameter of 0.78 meters, a takeoff weight of 900 kilograms and a takeoff thrust of 1.5 MN. The engines were alcohol fueled with liquid oxygen as an oxidant. The first launch of the A5 took place in the summer of 1938 at Greifswalder Oie. The first successful guided flights were in October 1939 in order to test the control systems planned for use in the A4. The A5 reached a ceiling of up to 12 kilometers and could be used several times.

External link

http://www.astronautix.com/lvs/a5.htm

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