RU2080015C1 - METHOD OF FLIGHT OF THE AIR-SPACE AIRPLANE WITH FILLING IN THE AIR - Google Patents
METHOD OF FLIGHT OF THE AIR-SPACE AIRPLANE WITH FILLING IN THE AIR Download PDFInfo
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- RU2080015C1 RU2080015C1 RU92014096/11A RU92014096A RU2080015C1 RU 2080015 C1 RU2080015 C1 RU 2080015C1 RU 92014096/11 A RU92014096/11 A RU 92014096/11A RU 92014096 A RU92014096 A RU 92014096A RU 2080015 C1 RU2080015 C1 RU 2080015C1
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- aircraft
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- fuel
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- composite
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Abstract
1. Способ полета воздушно-космического самолета с дозаправкой в воздухе, включающий старт воздушно-космического самолета с частичным запасом топлива для бортового двигателя, старт вспомогательного самолета-танкера, встречу самолетов в воздухе, соединение топливных систем самолетов, перекачивание топлива с борта самолета-танкера на борт воздушно-космического самолета, разъединение топливных систем самолетов с последующим их разведением для самостоятельного полета, отличающийся тем, что перед соединением топливных систем самолеты состыковывают жесткой механической связью в единый составной летательный аппарат, в процессе перекачивания топлива увеличивают полную механическую энергию составного летательного аппарата, а после разъединения топливных систем самолетов их вновь расстыковывают на самостоятельные самолеты.2. Способ по п.1, отличающийся тем, что увеличение полной механической энергии составного летательного аппарата осуществляют за счет увеличения его высоты.3. Способ по п.1, отличающийся тем, что увеличение полной механической энергии составного летательного аппарата осуществляют за счет увеличения его скорости.1. A method of flight of an aerospace aircraft with air refueling, including the launch of an aerospace aircraft with a partial supply of fuel for the onboard engine, launching an auxiliary tanker aircraft, meeting aircraft in the air, connecting aircraft fuel systems, pumping fuel from a tanker aircraft on board an aerospace aircraft, disconnecting the fuel systems of aircraft with their subsequent separation for independent flight, characterized in that before connecting the fuel systems, the aircraft are docked with a rigid mechanical connection into a single composite aircraft, in the process of pumping fuel, the total mechanical energy of the composite aircraft is increased, and after the separation of the aircraft fuel systems, they are again undocked into independent aircraft. 2. The method according to claim 1, characterized in that the increase in the total mechanical energy of the composite aircraft is carried out by increasing its height. The method according to claim 1, characterized in that the increase in the total mechanical energy of the composite aircraft is carried out by increasing its speed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU92014096/11A RU2080015C1 (en) | 1992-12-24 | 1992-12-24 | METHOD OF FLIGHT OF THE AIR-SPACE AIRPLANE WITH FILLING IN THE AIR |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU92014096/11A RU2080015C1 (en) | 1992-12-24 | 1992-12-24 | METHOD OF FLIGHT OF THE AIR-SPACE AIRPLANE WITH FILLING IN THE AIR |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU92014096A RU92014096A (en) | 1997-01-27 |
| RU2080015C1 true RU2080015C1 (en) | 1997-05-20 |
Family
ID=48434926
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU92014096/11A RU2080015C1 (en) | 1992-12-24 | 1992-12-24 | METHOD OF FLIGHT OF THE AIR-SPACE AIRPLANE WITH FILLING IN THE AIR |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2080015C1 (en) |
-
1992
- 1992-12-24 RU RU92014096/11A patent/RU2080015C1/en active
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