Rocket engine used in a German V-2 missile during World War II.
A V-2 (A-4) on a test stand at Peenemunde, Germany, during the war. It carried a 2,000pound warhead at speeds of about 3,600 mph and had a range of about 220 miles. The high, arching flight of the V2 carried it to an attitude of about 100 miles.
Launch of the V-2. The Germans, under the technical direction of Wernher von Braun, developed the V-2 rocket at their Peenemunde Research Facility. The 46-foot rocket used alcohol and liquid oxygen as fuel and could carry a 1,650-pound warhead 225 miles.
The German team of specialists that came to the United States after the war was initially assigned to Fort Bliss, Texas, where they reassembled and tested V-2 rockets brought to the United States from Germany. Later they went to Redstone Arsenal in Huntsville, Alabama.
The V-2 (A4) Ballistic Missile Technology
The V-2 was the first ballistic missile used in warfare and a significant advancement in rocket technology. Also known as the A4, it was developed by Nazi Germany during World War II and used against the Allies, primarily as a terror weapon. Because it was so inaccurate (it could barely hit a city-size target), it could not be used against specific military targets and was instead used against civilians who had no defense against it as it came screaming down from the upper atmosphere. Adolf Hitler named it his "Vengeance Weapon 2"or "V-2" because it wreaked vengeance upon a helpless population. (The "Vengeance Weapon 1," or "V-1", was a cruise missile.)
Despite its relative inaccuracy, the V-2 incorporated several major technological advances in rocketry. Its engine was 17 times more powerful than the largest rocket motor constructed up to that time; it flew at five times the speed of sound; and it could still fly relatively accurately to targets nearly 190 miles (306 kilometers) away.
Work began on the A4 in 1940 but proceeded slowly at first. The rocket team employed some of the best aerodynamicists in Germany, who conducted systematic tests on subscale models. In August 1941, Hitler ordered the completion of development of the A4 and the production of several hundred test and pre-production vehicles. Testing occurred during 1941, when tests of the large engine required for the rocket kept ending in explosions.
The A4 incorporated four major advances: its powerful engine, its aerodynamic shape, its innovative guidance system, and its radio transmission system. Together, these produced a terrifying weapon that ultimately had little military value to the Germans.
The rocket engine was fueled by an alcohol and water combination, with liquid oxygen serving as an oxidizer that enabled the fuel to burn, just as oxygen enables wood to burn. The fuel and oxidizer were pumped into a main combustion chamber where they mixed and then ignited, producing 56,000 pounds (249,100 newtons) of thrust, which escaped out of the rocket nozzle at the tail of the vehicle.
The engine contained a number of key technological innovations that enabled it to achieve significantly higher thrust. First, it had a new type of fuel nozzle for injecting the watered alcohol into the engine. These nozzles sprayed the fuel out in a rotational pattern that caused it to atomize better (in other words, create very small fuel droplets that had more surface area, like the water coming out of a spray bottle) so that it mixed better with the oxidizer and therefore burned more efficiently.
A second innovation was the use of a pre-chamber system that mixed the propellant and oxidizer in small chambers above the main combustion chamber. This produced better mixing before burning and kept the flames farther from the nozzles, preventing heat damage to the nozzles.
A third innovation was the use of a shorter, rounder combustion chamber, which mixed the propellants better than an earlier design with a longer chamber. The final innovation was the rocket exhaust nozzle. Previous nozzles had a 10-12-degree angle of opening between the sides of the cone, resulting in a long, thin cone. But the A4 engine had a nozzle with an angle of 30 degrees. This reduced friction between the exhaust gases and the wall and also resulted in a shorter nozzle.
Because the rocket would travel so fastfaster than any other object at that timeits aerodynamic shape was very important, particularly the fins for controlling the rocket. But determining the proper shape was difficult because no wind tunnel existed at the time that could test objects at such high speeds. The Germans built a world-class aerodynamic institute at their rocket test center at Peenemünde, with several supersonic wind tunnels. These tunnels were not ready in time, however, and many of the key decisions concerning the A4's shape were made from educated guesses and confirmed later. For instance, the unusual rounded shape of the A4 (when compared with modern rockets) was due to the fact that it was based on the shape of a rifle bullet. Designers figured that since a rifle bullet flew through the air without tumbling, a rocket using the same shape would do the same.
The third primary technological advance of the A4 was in the area of guidance. Early rockets had no guidance system at all and could be aimed only in a general direction. Later, some simple guidance systems were adopted that directed rockets to pitch over in flight to aim toward a target. But the A4 had to fly a long distance with some degree of accuracy to hit its target, so it required a system for pointing it in the right direction and shutting off the engine once the proper velocity was achieved. This was achieved through the use of what is called an inertial guidance system, a system in which a stabilized platform remains fixed in space regardless of how the vehicle moves around it. This stabilized platform allows for measuring the position or acceleration of the vehicle, since the platform remains pointed in one direction and the changes in the vehicle can be measured compared to the stable platform. In the middle of the rocket exhaust were four vanes that were used to deflect the thrust and steer the rocket based upon commands from the guidance unit. The A4 system was significantly more advanced than previous guidance systems. Still, despite this advanced system, the A4 could hit only a city-sized target from 190 miles (306 kilometers) away.
A fourth advance was the development of a radio transmission system that could relay information about the missile's performance to the ground. Earlier test missiles used a movie camera to record an oscilloscope, which was a device that projected a wave on a screen indicating the rocket's performance. The film was then retrieved when the rocket splashed down. But because the A4 test flights would cover hundreds of miles and recovery was nearly impossible, the engineers needed a means of "tele-metering" information to a ground station. This development, now referred to as telemetry, became common to all rocket test programs, as well as to many aircraft test programs.
The A4 was 46 feet (14 meters) long and five feet (1.5 meters) in diameter at its thickest spot. Its fins spanned nearly 12 feet (3.7 meters) at the base of the rocket, and it weighed 45,000 pounds (20,412 kilograms). It had a 2,000-pound (907-kilogram) warhead that stayed attached to the rocket throughout flight, and the entire missile crashed down on its target. Its first successful flight was on October 3, 1942.
Thousands of A4/V-2 rockets were fired during the war. After the war ended, many members of the rocket team that developed the A4, including Wernher von Braun, went to the United States or the Soviet Union and assisted in the development of these countries' ballistic missile programs.
--Dwayne A. Day
Sources and Further Reading:
Hölsken Dieter. V-Missiles of the Third Reich, The V-1 and V-2. Hong Kong: Monogram Aviation Publications, 1994.
Johnson, David. V-1, V-2: Hitler's Vengeance on London. Chelsea, Mich.: Scarborough House, 1991.
Longmate, Norman. Hitler's Rockets: the Story of the V-2s. London: Hutchinson, 1985.
Neufeld, Michael, The Rocket and the Reich. New York: The Free Press, 1995.
Winter, Frank H. Rockets Into Space. Cambridge, Mass.: Harvard University Press, 1990.
"The Evolution of the Rocket." http://www-istp.gsfc.nasa.gov/stargaze/Srockhis.htm
"V-2 Rocket." White Sands Missile Range. Public Affairs Office. http://www.wsmr.army.mil/paopage/Pages/V-2.htm