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Europe 1934 stock footage and images
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Various designs for self-cooling rocket motors, by Professor Eugen Sänger, and test of the S.R.5 motor in 1934
Professor Eugen Sänger's design for self-cooling rocket motor, March 20, 1934. Drawing of Rocket motor S.R.4, from April 14, 1934, designed with a cooling coil around the combustion chamber jacket. Drawing of Motor S.R.5, from April 24, 1934, with exits in the combustion chamber and nozzle only from cooling coils. Picture of the S.R.5 motor. Sänger's drawings for a self-demanding pumping head in single and double piston designs. Such a rocket motor, designed on May 13, 1934, to generate 100 Kg of thrust. Pictures of the S.R.5 rocket motor and test apparatus, with it firmly fastened to a steel plate to keep it from moving during the burn test. Closeup of the actual burn test in Professor Sänger's workshop, Vienna Austria.
Rocket research and development work carried on by Richard Tiling, in Germany, after death of his brother, Reinhold Tiling
Following his death in 1933, Reinhold Tiling's work on rocketry was carried forward by his brother, Richard, who successfully worked on perfecting projectile missiles,and especially on improving the explosion safety of propellants, during 1934. A photograph of several rockets is shown, followed by a series of animated design sketches. Slate refers to Swirl nozzle provided with rotating projectile in describing one sketch. Another is described as Richard Tiling's design of Projectile missiles to shoot down aircraft. Richard Tiling and assistants are shown standing over many rocket projectiles in preparation for a demonstration before the Navy and the Army Ordnance Department in Meppen on April 17, 1934 (in which they were shot distances reaching 12 thousand meters). View of a 10 centimeter rocket on its launching stand. Richard Tiling and assistants placing a missile on a stand. Views of 10 and 15 centimeter missiles at a demonstration in Cuxhaven in Summer, 1934. The missiles are shown on the ground. Launching stand for direct and indirect fire with special "Dickkopf" missile. Catapult launch frame for 10 and 15 centimeter projectiles in April, 1934. Photograph of a 10 cm projectile being fired.
Helen Mack wins the title "The American Beauty" in New York, United States.
Scenes from the "The American Queen of Beauty ' pageant in New York City, United States, in October 1934. (The "Miss America" pageant was not held in 1934 due to Great Depression financial troubles that affected the pageant in 1933. This "American Queen of Beauty" pageant was sponsored by Madison Square Garden, and held only this one time, in 1934). Contestants in swim suits move around the judges. The judges consisting of experts are seated on the center of the stage. Helen Mack, who was Miss New York State, is seen being given the title of American Queen of Beauty after she defeated 3,000 girls from 30 states. She holds the silver winner's cup.
Contributions to rocket research by German Professor Eugen Sänger in the 1930s
German Professor Eugen Sänger conceived of a rocket-propelled airplane in 1934. View of his sketches and notes.View of a workshop, close to his home, where Sänger developed his ideas. It is a nondescript building with wooden exterior and "Deutsche Raketenflug-Werft, Vien1934" (German Rocketflight shipyard, Vienna,1934) scrawled on its door. Professor Sänger and an assistant are seen in doorway of the workshop. Interior views of machinery. Blueprint cross-section of Sängers first Rocket motor (the S.R.1) from 1932. Drawing of test facility arrangement from 1932. Drawing of the S.R.2 rocket motor from 1933, with high pressure liquid oxygen cooling. Drawing of testing apparatus and arrangement from 1933, including Bosch fuel injection pump.
Professor Eugen Sänger's ideas for using rockets in national defense and space exploration
Drawings and pictures of Professor Eugen Sänger's S.R.13 and 14 Rocket motors from September, 1934. He holds a motor in his hand and points out its features. Photograph of Austrian patent certificate number 144809 issued to Doctor Eugen Sänger in Vienna, effective September 15, 1935, for Rocket engine and method for its operation. Glimpse of illustrations in the document. Drawing of planned 500 Kg thrust rocket motor designed by Sänger Rocket Motors. Eugen Sänger's drawings for a rocket-propelled missile to hunt airplanes. Design of a rocket motor (the S.R.X), on June 10, 1934, with 1000 kg thrust for a tropospheric experimental aircraft. Image of a letter to Dr.Sänger, from the the Federal Ministry of National Defense, dated February 3, 1934, stating that his ideas were not practially realizable.
Rocket motor designs by International scientists and inventors, reflecting early work by German rocket researchers
Designs by various international scientists and inventors who have contributed to solving the problems of rocket motor development, based on the German preparatory work. Their combustion chamber designs owe much to the German pioneers in the field. Shown are design sketches by Russian scientist, Konstantin Tsiolkovsky (Ziolkowsky) in 1914; French inventor Henri Melot, in 1920; German Friedrich Zander, in 1931; Bull, 1932; The American Rocket Society, with several designs from 1932; and The Cleveland Rocket Society. Views of rocket combustion research activity by Ernst Loebell of the Cleveland Rocket Society in 1933. He is seen outdoors in the snow with his apparatus. View of Loebell's test firing stand, and a picture of an actual test firing, outdoors. Ernst Loebell with model and rocket motor from his spaceship projects of 1934 and at the International Exposition dedicated to Art and Technology in Modern Life held in Paris, 1937. Cutaway views of the spaceship. The rocket motor wrapped in cooling coils. Rocket motor design by John Shesta of the American Rocket Society, from 1934. Design by Rene Armengaud of France, in 1934 and Deich in 1935.
