Aggregate 9 (A-9)
Aggregate 10 (A-10)

Surface-to-Surface Missile

Service Data

In Service:

Production Data

First Flight:
Manufacturer: Peenemünde
Number built:

Technical Data

Type: Surface-to-Surface Missile

Guidance system: Gyroscope
Length: 26 m
Wingspan: m
Diameter: 4.75 m
Weight: 100 tons
Engine: first stage 1 × liquid fuel rocket engine producing up to to 30,500 kg of thrust. second stage 1 × liquid fuel rocket engine producing up to to 152,500 kg of thrust
Maximum speed: 7,680 km/h
Range: 4,800 km
Warhead:
Fuze:
Launch Platform: Mobile
Operators: Heer
Variants:
A-1
A-2
A-3
A-4
A-4 SLBM
A-4b / A-9
A-5
A-6
A-7
A-8
A-9 / A-10

Other: Missiles
Articles:

History

The Aggregate 9 (A-9) / Aggregate 10 (A-10) was the last in the Aggregate series of missile designed and developed by Dr.-Ing. Wernher von Braun in 1944 under the leadership of Dr. Walter Robert Dornberger, at Army Research Center Peenemünde.

The Aggregate 9 (A-9) / Aggregate 10 (A-10) was a two-stage intercontinental ballistic missile (ICBM) which design can be traced back to the early 1940s some of the people who assisted in the design were Ludwig Roth, Hermann Oberth, Walter Thiel. However work resumed in 1944, under the codename of Projekt Amerika. The Aggregate 9 (A-9) / Aggregate 10 (A-10) was 26 m long by 4.75 m in diameter and had a take off weight 100 tons and used the following engines first stage 1 × liquid fuel rocket engine producing up to to 30,500 kg of thrust. second stage 1 × liquid fuel rocket engine producing up to to 152,500 kg of thrust. Which gave a maximum thrust of 183,500 kg for 50 seconds of burn time

Gallery

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Sources

The Warplanes of the Third Reich.
ISBN-10: 0385057822

German Aircraft of the Second World War.
ISBN-10: 0370000242

Hitler's Luftwaffe.
ISBN-10: 051718771X

For a complete list of sources