SYSTEM FOR SEPARATING PAYLOAD FROM SPACE VEHICLE BOARD Russian patent published in 2013 - IPC B64G1/64 F42B15/36 

Abstract RU 2471684 C1

FIELD: transport.

SUBSTANCE: invention relates to space engineering, namely to devices for docking payload to main spacecraft and payload separating after insertion to design orbit. System for separating payload includes disengageable adapter installed between structures of aircraft and payload and containing mechanical locks with retaining and fixing elements, mechanical locks fixation device. The system has pushers for payload separation. The mechanical locks fixation device is made as equal-arm rocker with unlimited number of arms corresponding to number of mechanical locks. The rocker is installed on rotation axis fixed in adapter housing Through adapter via-windows, the equal-arm rocker is pivotally interacting by means of tie-rods with fixing elements of mechanical locks the spring-loaded rods of which have recess for retaining rotating double-arm lever by other end interacting with fixing element of lock. One of arms of the equal-arm rocker is pivotally interacting via tie-rod with spring pusher, the other arm - with explosive pin which are rigidly fixed on the outside of adapter housing. On a payload, arresting devices are made which interact with spring-loaded rods of mechanical locks.

EFFECT: higher reliability of docking and separating system operation.

4 dwg

Similar patents RU2471684C1

Title Year Author Number
DEVICE FOR CONTROLLED LUNCHING OF NANO- AND MICROSATELLITES 2014
  • Filonin Oleg Vasil'Evich
  • Belokonov Igor' Vital'Evich
  • Talyzin Jurij Borisovich
RU2551408C1
DEVICE FOR SPACE APPARATUS SEPARATION 2010
  • Kruglov Genrikh Evgen'Evich
  • Novikov Valentin Nikolaevich
  • Moiseev Valentin Petrovich
  • Solunin Vladimir Sergeevich
  • Cherkashina Ljubov' Vjacheslavovna
RU2453481C1
PAYLOAD SEPARATION SYSTEM 2009
  • Tolmachev Sergej Mikhajlovich
  • Ivanov Vladimir Konstantinovich
  • Soin Valerij Ivanovich
RU2396191C1
SYSTEM OF SEPARATION OF PAYLOAD OF SPHERICAL SHAPE 2003
  • Drozhzhin Vladimir Semenovich
  • Podzorov Valerij Nikolaevich
  • Murashov Vladimir Vasil'Evich
RU2276046C2
PAYLOAD SEPARATION SYSTEM 2003
  • Kiriljuk Anatolij Ivanovich
  • Podzorov Valerij Nikolaevich
  • Evteev Aleksandr Nikolaevich
  • Murashov Vladimir Vasil'Evich
RU2268208C2
UNIT OFFICES AND OPENING THE VALVES OF SOLAR BATTERIES OF SPACECRAFT 2010
  • Afanas'Ev Anatolij Petrovich
  • Bil'Ko Viktor Vasil'Evich
RU2441817C1
SPACECRAFT SEPARATION SYSTEM 2014
  • Voronin Evgenij Aleksandrovich
  • Grebnev Nikolaj Egorovich
  • Kruglov Genrikh Evgen'Evich
  • Moiseev Valentin Petrovich
  • Solunin Vladimir Sergeevich
  • Filatov Sergej Anatol'Evich
RU2564457C1
PAYLOAD SEPARATION SYSTEM 2005
  • Abushenko Sergej Nikolaevich
  • Evteev Aleksandr Nikolaevich
  • Kasatkin Gennadij Mikhajlovich
  • Kiriljuk Anatolij Ivanovich
  • Podzorov Valerij Nikolaevich
RU2293694C1
INFLATABLE DEVICE OF PASSIVE DECELERATION SYSTEM OF LAST STAGE OF LAUNCH VEHICLE 2000
  • Majorov Ju.N.
  • Dukin A.D.
RU2199474C2
CARRIER ROCKET DETACHABLE NOSE CONE 2010
  • Grebnev Nikolaj Egorovich
  • Kruglov Genrikh Evgen'Evich
  • Novikov Valentin Nikolaevich
  • Moiseev Valentin Petrovich
  • Solunin Vladimir Sergeevich
  • Shemendjuk Vjacheslav Mitrofanovich
RU2428359C1

RU 2 471 684 C1

Authors

Tkach Vasilij Efimovich

Kruglov Genrikh Evgen'Evich

Starodubtseva Elena Valer'Evna

Moiseev Valentin Petrovich

Filatov Sergej Anatol'Evich

Dates

2013-01-10Published

2011-05-31Filed