Original Romanian Research for a Rocket Engine with Multiple Combustion Chambers during 1940 - 1944
The paper presents certain points of view regarding the history of Romanian rocket engines, during 1940-1944. Working independently of other scientists, during 1942 – 1944 the Romanian Nicolae Văideanu has invented and designed, independently of other researchers, a liquid fuel missile called UDOVIL...
| الحاوية / القاعدة: | INCAS Bulletin |
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| المؤلفون الرئيسيون: | , , |
| التنسيق: | مقال |
| اللغة: | الإنجليزية |
| منشور في: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2020-03-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://bulletin.incas.ro/files/zaganescu-n-f__gheorghe-c-m__kalmutchi__vol_12_iss.pdf |
| الملخص: | The paper presents certain points of view regarding the history of Romanian rocket engines, during 1940-1944. Working independently of other scientists, during 1942 – 1944 the Romanian Nicolae Văideanu has invented and designed, independently of other researchers, a liquid fuel missile called UDOVILUL-V [3]. According to the design drawings, this missile was equipped with aerodynamically profiled propelling nozzles and was provided with a special alternator – distributor, the bypass valve adjusting the fuel components dosage in the two combustion chambers, in fuel tanks and pipes, while a special designed gas turbine was driving the centrifugal pumps and other mechanical equipment. Within his main patent the Romanian inventor has included the design of several components [2], [4], [5]. The technical solution of this outstanding design in rocketry development could provide 20kN thrust after 60 sec, enabling a speed of 3200 km/h [10]. |
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| تدمد: | 2066-8201 2247-4528 |