FIELD: space engineering; deployment of cable system in form of cluster of two objects. SUBSTANCE: two objects connected by cable are disconnected and separation speed is imparted to at least one of them along local vertical, after which cable is extended and force of its tension is regulated by the following law: Np= A•V/(1-B•L/Lf),, where Np is preset force of tension of rope: V is cable extending speed; L is present length of extended part of cable; Lf is preset final length of cable: A and B are constant positive and B is lesser than one. Cable extending is discontinued at the moment when its length gets equal to preset final length. EFFECT: facilitated procedure. 1 dwg , 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF DEPLOYMENT OF ORBITAL CABLE SYSTEM | 1996 |
|
RU2112715C1 |
| STAND FOR GROUND TEST OF DEPLOYMENT OF ORBITAL CABLE SYSTEM AND METHOD OF CONTROL OF THIS STAND (VERSIONS) | 1999 |
|
RU2164885C1 |
| DEVICE FOR RELEASE OF CABLE OF TWO-SPACECRAFT CLUSTER AND CONTROL SYSTEM | 1999 |
|
RU2148535C1 |
| DEPLOYMENT OF SPACE ROPE SYSTEM AT DELIVERY OF LANDER FROM ORBITAL STATION TO GROUND | 2014 |
|
RU2564930C1 |
| LONG-ENDURANCE MANNED ORBITAL CABLE COMPLEX | 1993 |
|
RU2088491C1 |
| METHOD OF DELIVERY OF LANDER FROM ORBITAL STATION TO EARTH BASED ON PASSIVE DEPLOYMENT OF SPACE CABLE SYSTEM | 2011 |
|
RU2497729C2 |
| LARGE-SIZE SPACE COLLAPSIBLE REFLECTOR | 1996 |
|
RU2101811C1 |
| METHOD OF DETERMINATION OF VELOCITY HEAD OF INCOMING FLOW ON BOARDS SPACE VEHICLE EQUIPPED WITH SYSTEM OF POWERED GYROSCOPES | 1992 |
|
RU2087390C1 |
| DEVICE FOR EJECTION OF DOCKING CABLE OF TWO SPACECRAFT (VERSIONS) | 2011 |
|
RU2482032C2 |
| SYSTEM FOR DETERMINATION OF CONTROL MOMENT AT TURN OF SPACE VEHICLE | 1995 |
|
RU2094332C1 |
