FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to repair of spacecraft. Device for rapid sealing of a breakdown hole in a body of a space object comprises a sealing element and a reservoir. Reservoir is made in the form of double-sided umbrella. One working inner side of the umbrella is made of strong propylene, and the second working outer side is made of thin sheet titanium. Sides of the umbrella are located on different sides from the shell of the spacecraft. Container comprises handle with retainer to open umbrella, part of handle located between two working sides of umbrella is equipped with nozzles. Handle is equipped with an inlet valve, to which a compressed air cylinder is connected. Handle passes through the puncheon hole. Reservoir is filled with a sealing element.
EFFECT: enabling the application scope expansion.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR SEALING OF DEFECTS OF SHELLS OF SPACECRAFTS | 2019 |
|
RU2721360C1 |
IMMEDIATE SEALING OF PUNCHED HOLE IN MANNED SPACESHIP BODY AND DEVICE TO THIS END | 2014 |
|
RU2568514C1 |
METHOD OF DETERMINING COORDINATES OF PUNCTURE OF HOUSING OF PRESSURE COMPARTMENT OF SPACE OBJECT WITH NATURAL OR MAN-MADE PARTICLE AND DEVICE THEREFOR | 2014 |
|
RU2583251C2 |
DEVICE FOR DETERMINATION OF POSITION COORDINATES OF MANNED SPACE OBJECT PRESSURE SKIN PUNCTURE BY SPACE PARTICLES AND METHOD FOR PUNCTURE POSITION COORDINATES DETERMINATION | 2008 |
|
RU2387966C1 |
DEVICE FOR DETERMINATION OF POSITION COORDINATES OF UNMANNED SPACE OBJECT PRESSURE SKIN PUNCTURE BY SPACE PARTICLES AND METHOD FOR PUNCTURE POSITION COORDINATES DETERMINATION | 2008 |
|
RU2387965C1 |
METHOD FOR EXPLORATION OF ICE SITUATION, USING REMOTELY CONTROLLED UNMANNED AERIAL VEHICLES, AND DEVICE FOR ITS IMPLEMENTATION | 2021 |
|
RU2778158C1 |
METHOD AND SYSTEM FOR NAVIGATION SUPPORT OF PILOTAGE AND POSITIONING | 2021 |
|
RU2773497C1 |
METHOD FOR INSTALLING A MARINE RANGE OF BOTTOM STATIONS | 2023 |
|
RU2797702C1 |
GREENHOUSE | 2021 |
|
RU2765488C1 |
METHOD OF MAINTAINING SPACESHIP TIGHTNESS IN COLLISION WITH HIGH-SPEED BODIES AND DEVICE TO THIS END (VERSIONS) | 2011 |
|
RU2479470C2 |
Authors
Dates
2019-11-19—Published
2019-03-11—Filed