FIELD: mechanics, transport.
SUBSTANCE: attachment device incorporated with spacecraft being detached from carrier rocket in orbit incorporates a hollow bolt with groove and locking blocks with external sleeve displaced with the help of drive. Note that aforesaid bolt is furnished with fast-action heater arranged in the bolt bore and connected to power supply.
EFFECT: higher reliability of spacecraft detachment, reduced impact loads on spacecraft.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
PYROLOCK WITH PYROGAS SHOCK ABSORPTION | 2007 |
|
RU2354923C1 |
DEVICE TO FIX AND SEPARATE PARTS OF STRUCTURE | 2013 |
|
RU2539710C1 |
DEVICE FOR HOLDING AND RELEASING TRANSFORMABLE MECHANICAL SYSTEMS OF SPACECRAFT | 2017 |
|
RU2714037C2 |
DEVICE FOR SEPARATION OF ROCKET STAGE AND SEPARABLE SPACE VEHICLE | 1996 |
|
RU2111905C1 |
HOLDER | 2013 |
|
RU2558960C2 |
DETONATION DEVICE FOR CONNECTION AND SUBSEQUENT SEPARATION OF ROCKET AND SPACECRAFT STRUCTURE ELEMENTS | 2019 |
|
RU2729494C1 |
SPACECRAFT UNDOCKING SYSTEM AND METHOD FOR ASSEMBLY AND INSTALLATION THEREOF | 2015 |
|
RU2586942C1 |
DEVICE FOR CONTAINMENT AND RELEASE OF EXPANDABLE ELEMENTS OF SPACECRAFT DESIGN | 2015 |
|
RU2619497C2 |
DOCKING UNIT OF DETACHABLE OBJECTS OF AIRCRAFTS | 2016 |
|
RU2628282C1 |
DEVICE FOR HOLDING AND RELEASING TRANSFORMED MECHANICAL SYSTEMS OF SPACECRAFT | 2017 |
|
RU2669246C1 |
Authors
Dates
2008-12-20—Published
2007-06-22—Filed