‎‎
‎ROCKET n°2‎

‎Liquid-Propellant Rocket Development (with 11 plates). - [THE WORLD'S FIRST LIQUID-FUELED ROCKET]‎

‎Washington, The Smithsonian Institution, 1936. 8vo. In recent red full cloth with gilt lettering to front board. Published as part of ""Smithsonian Miscellaneous Collections, Volume 95, Number 3, Publication 3381"". A fine and clean copy. (2), 10 pp. + 11 photographic plates.‎

‎First edition of Goddard's paper on liquid-fueled rocket development. Goddard is credited with creating and building the world's first liquid-fueled rocket and is often referred to as the man who ushered in the Space Age (Pendray, Rocket Development). By temperament and training Goddard was not a team worker, yet he laid the foundation from which team workers could launch men to the moon"" (DSB). Goddard was secretive about his research and only published two papers"" ""A Method of Reaching Extreme Altitudes"" (1919) and the present. Goddard launched the first liquid-fuel rocket on 16 March 1926 near Auburn, Mass. The ten-foot rocket, nicknamed ""Nell"" reached an altitude of 41 feet, traveled a distance of 184 feet and landed 2.5 seconds after lift-off in a cabbage patch. ""Although his list of firsts in rocketry was distuguished, Goddard was eventually surpassed by teams of rocket research and development experts elsewhere, particularly in Germany."" (DSB).""Like the Russian hero Konstantin Tsiolkovsky and the German pioneer Hermann Oberth, Goddard worked out the theory of rocket propulsion independently [...] Having explored the mathematical practicality of rocketry since 1906 and the experimental workability of reaction engines in laboratory vacuum tests since 1912, Goddard began to accumulate ideas for probing beyond the Earth's stratosphere. His first two patents in 1914, for a liquid-fuel gun rocket and a multistage step rocket, let to some modest recognition and financial support from the Smithsonian Institution [...] With an eye toward patentability of demonstrated systems and with the aid of no more than a handful of technicians, Goddard achieved a series of workable liquid-fuel flights starting in 1926. Through the patronage of Charles A. Lindbergh, the Daniel and Florence Guggenheim Foundation, and the Carnegie and Smithsonian institutions, the Goddards and their small staff were able to move near Roswell, New Mexico. There, during most of the 1930s, Goddard demonstrated, despite many failures in his systematic static and flight tests, progressively more sophisticated experimental boosters and payloads, reaching speeds of 700 miles per hour and altitudes above 8000 feet in several test flights"" (DSB).‎

‎Liquid-Propellant Rocket Development (with 11 plates). - [THE WORLD'S FIRST LIQUID-FUELED ROCKET]‎

‎Washington, The Smithsonian Institution, 1936. 8vo. In recent red full cloth with gilt lettering to front board. Published as part of ""Smithsonian Miscellaneous Collections, Volume 95, Number 3, Publication 3381"". A fine and clean copy. (2), 10 pp. + 11 photographic plates.‎

‎First edition of Goddard's paper on liquid-fueled rocket development. Goddard is credited with creating and building the world's first liquid-fueled rocket and is often referred to as the man who ushered in the Space Age (Pendray, Rocket Development). By temperament and training Goddard was not a team worker, yet he laid the foundation from which team workers could launch men to the moon"" (DSB). Goddard was secretive about his research and only published two papers"" ""A Method of Reaching Extreme Altitudes"" (1919) and the present. Goddard launched the first liquid-fuel rocket on 16 March 1926 near Auburn, Mass. The ten-foot rocket, nicknamed ""Nell"" reached an altitude of 41 feet, traveled a distance of 184 feet and landed 2.5 seconds after lift-off in a cabbage patch. ""Although his list of firsts in rocketry was distuguished, Goddard was eventually surpassed by teams of rocket research and development experts elsewhere, particularly in Germany."" (DSB).""Like the Russian hero Konstantin Tsiolkovsky and the German pioneer Hermann Oberth, Goddard worked out the theory of rocket propulsion independently [...] Having explored the mathematical practicality of rocketry since 1906 and the experimental workability of reaction engines in laboratory vacuum tests since 1912, Goddard began to accumulate ideas for probing beyond the Earth's stratosphere. His first two patents in 1914, for a liquid-fuel gun rocket and a multistage step rocket, let to some modest recognition and financial support from the Smithsonian Institution [...] With an eye toward patentability of demonstrated systems and with the aid of no more than a handful of technicians, Goddard achieved a series of workable liquid-fuel flights starting in 1926. Through the patronage of Charles A. Lindbergh, the Daniel and Florence Guggenheim Foundation, and the Carnegie and Smithsonian institutions, the Goddards and their small staff were able to move near Roswell, New Mexico. There, during most of the 1930s, Goddard demonstrated, despite many failures in his systematic static and flight tests, progressively more sophisticated experimental boosters and payloads, reaching speeds of 700 miles per hour and altitudes above 8000 feet in several test flights"" (DSB).‎

‎Rocket Ballistic Data. Fin-stabilized and Spin-stabilized Rockets. - [RESTRICTED REPORT ON BALLISTIC ROCKET-CURVES]‎

‎California, California Institute of Technology, 1946. Royal8vo. In the original blue full cloth. Minor wear to extrimities, othervise a very fine and clean copy. XIV, 406 pp.‎

‎First printing of this restricted report on ballistic rocket-curves. The back of half title states that: ""This document contains information affecting the National Defense of the United States within the meaning of the Espionage Act, U.S.C. 50"" 31 and 32. Its transmission of the revelation of its contents in any manner to an unauthorized person is prohibited by law."" The report contains a ballistic analysis of 65 different types of rocket from chemical warfare rockets, demolition rockets to forward-firing aircraft rockets and rocket grenades. ‎

‎Barrer M., Jomotte A., Webeck W., Vandenkerkhove J. Rocket engines. In Russi‎

‎Barrer M., Jomotte A., Webeck W., Vandenkerkhove J. Rocket engines. In Russian /Barrer M., Zhomott A., Vebek V., Vandenkerkkhove Zh. Raketnye dvigateli. In Russian. The book is devoted mainly to the theory, calculation and design of liquid and solid propellant rocket engines. Separate chapters of the book also consider the characteristics and properties of solid and liquid propellants for rocket engines, as well as the equipment for testing these engines. We have thousands of titles and often several copies of each title may be available. Please feel free to contact us for a detailed description of the copies available. SKUalb8569e0613b5d7118‎

‎A sergeants manual for rocket forces and artillery. For commanders of artiller‎

‎A sergeants manual for rocket forces and artillery. For commanders of artillery guns, mortars and rocket-propelled vehicles. In Russian /Uchebnik serzhanta raketnykh voysk i artillerii. Dlya komandirov orudiy, minometov i boevykh mashin reaktivnoy artillerii. Approved by the Chief of Rocket Forces and Artillery of the Land Forces. Editor N. V. Danilenkov. M. Voenizdat, 1989. 224s. We have thousands of titles and often several copies of each title may be available. Please feel free to contact us for a detailed description of the copies available. SKUalb988a71fd28e457b5.‎