RU97115019A - METHOD FOR PERFORMING VERTICAL TAKEOFF BY A SPEED AIRCRAFT - Google Patents

METHOD FOR PERFORMING VERTICAL TAKEOFF BY A SPEED AIRCRAFT

Info

Publication number
RU97115019A
RU97115019A RU97115019/28A RU97115019A RU97115019A RU 97115019 A RU97115019 A RU 97115019A RU 97115019/28 A RU97115019/28 A RU 97115019/28A RU 97115019 A RU97115019 A RU 97115019A RU 97115019 A RU97115019 A RU 97115019A
Authority
RU
Russia
Prior art keywords
parachute
aircraft
cable
performing vertical
vertical takeoff
Prior art date
Application number
RU97115019/28A
Other languages
Russian (ru)
Other versions
RU2121941C1 (en
Inventor
Б.П. Таланов
Original Assignee
Б.П. Таланов
Filing date
Publication date
Application filed by Б.П. Таланов filed Critical Б.П. Таланов
Priority to RU97115019A priority Critical patent/RU2121941C1/en
Priority claimed from RU97115019A external-priority patent/RU2121941C1/en
Application granted granted Critical
Publication of RU2121941C1 publication Critical patent/RU2121941C1/en
Publication of RU97115019A publication Critical patent/RU97115019A/en

Links

Claims (2)

1. Способ выполнения вертикального взлета скоростным летательным аппаратом, включающий вывод парашюта на тросе в вертикальном направлении, отличающийся тем, что парашют закрепляют на средстве его вывода, например ракеты, второй конец троса парашюта закрепляют на шкиве с приводом, соединяют хвостовую часть летательного аппарата с площадкой взлета, запускают двигатель и выводят парашют до натяжения его троса, а после достижения тяги двигателем, достаточной для осуществления полета, втягивают парашют со скоростью, которая обеспечивает подъем летательного аппарата над площадкой взлета и освобождают трос хвостовой части.1. The method of performing vertical take-off by a high-speed aircraft, including the output of the parachute on the cable in the vertical direction, characterized in that the parachute is fixed to the means of its output, for example rockets, the second end of the parachute cable is mounted on a pulley with a drive, the tail part of the aircraft is connected to the platform take-off, they start the engine and put out the parachute until the cable is pulled, and after reaching the engine thrust sufficient for the flight, the parachute is pulled in at a speed that ensures em aircraft on take-off pad and release the rope tail. 2. Способ по п. 1, отличающийся тем, что трос парашюта соединяют с летательным аппаратом между центром масс и носовой частью его. 2. The method according to p. 1, characterized in that the parachute cable is connected to the aircraft between the center of mass and its bow.
RU97115019A 1997-09-02 1997-09-02 Method of performance of vertical take-off by high-speed flying vehicle RU2121941C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97115019A RU2121941C1 (en) 1997-09-02 1997-09-02 Method of performance of vertical take-off by high-speed flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97115019A RU2121941C1 (en) 1997-09-02 1997-09-02 Method of performance of vertical take-off by high-speed flying vehicle

Publications (2)

Publication Number Publication Date
RU2121941C1 RU2121941C1 (en) 1998-11-20
RU97115019A true RU97115019A (en) 1999-06-27

Family

ID=20196954

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97115019A RU2121941C1 (en) 1997-09-02 1997-09-02 Method of performance of vertical take-off by high-speed flying vehicle

Country Status (1)

Country Link
RU (1) RU2121941C1 (en)

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