RU97113362A - METHOD FOR RUNNING THE OBJECT FROM THE AIRCRAFT - Google Patents

METHOD FOR RUNNING THE OBJECT FROM THE AIRCRAFT

Info

Publication number
RU97113362A
RU97113362A RU97113362/28A RU97113362A RU97113362A RU 97113362 A RU97113362 A RU 97113362A RU 97113362/28 A RU97113362/28 A RU 97113362/28A RU 97113362 A RU97113362 A RU 97113362A RU 97113362 A RU97113362 A RU 97113362A
Authority
RU
Russia
Prior art keywords
parachute
cable
rocket
aircraft
roller
Prior art date
Application number
RU97113362/28A
Other languages
Russian (ru)
Other versions
RU2120890C1 (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 RU97113362A priority Critical patent/RU2120890C1/en
Priority claimed from RU97113362A external-priority patent/RU2120890C1/en
Application granted granted Critical
Publication of RU2120890C1 publication Critical patent/RU2120890C1/en
Publication of RU97113362A publication Critical patent/RU97113362A/en

Links

Claims (1)

Способ спуска объекта о летательного аппарата, включающий в себя аэродинамическое взаимодействие с набегающим потоком воздушной массы, соединенного со спусковым объектом парашютом, отличающийся тем, что парашют и ракету соединяют через ролик и тормоз на спускаемом объекте тросом, а над парашютом закрепляют дополнительную ракету со связью, которая обрывается при натяжении участка между роликом и тормозом после запуска дополнительной ракеты, при этом между роликом и парашютом оставляют свободную часть троса, обеспечивающую эффективное торможение при свободном падении, затем выводят всю систему за борт летательного аппарата, включают ракеты и после отрыва ракеты парашюта и натяжения троса ракеты на другом от парашюта конце троса, изменяют степень торможения до получения торможения спуска.A method of launching an object about an aircraft, including aerodynamic interaction with an incoming air mass flow, connected by a parachute to the trigger object, characterized in that the parachute and the rocket are connected via a roller and brake to the launched object by a cable, and an additional rocket is fixed above the parachute with a connection, which breaks off when the section is pulled between the roller and the brake after the launch of an additional rocket, while the free part of the cable is left between the roller and the parachute, which ensures effective braking during a free fall, then the entire system is taken overboard of the aircraft, the rockets are turned on, and after the rocket is torn off the parachute and the cable is pulled at the other end of the cable from the parachute, the degree of braking is changed until the launch is braked.
RU97113362A 1997-08-05 1997-08-05 Method of descent of object from flying vehicle RU2120890C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97113362A RU2120890C1 (en) 1997-08-05 1997-08-05 Method of descent of object from flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97113362A RU2120890C1 (en) 1997-08-05 1997-08-05 Method of descent of object from flying vehicle

Publications (2)

Publication Number Publication Date
RU2120890C1 RU2120890C1 (en) 1998-10-27
RU97113362A true RU97113362A (en) 1999-06-20

Family

ID=20196018

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97113362A RU2120890C1 (en) 1997-08-05 1997-08-05 Method of descent of object from flying vehicle

Country Status (1)

Country Link
RU (1) RU2120890C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU7782601A (en) * 2000-08-08 2002-03-22 Yusupovich Khalidov Hamid Aparc system for air passengers and load rescue

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