FIELD: aviation.
SUBSTANCE: landing aid comprises landing supports with the central racks containing the master cylinder with a cell energy sink and attaching lug to the spacecraft body, telescopic rod with extension mechanism, bearing tarel pivotally connected with a telescopic rod. Landing gear is equipped with ropes made of high modulus material. Pneumatic sliding fence rod is connected to the master cylinder and the housing - with a transverse beam fixed in the recess of the landing gear.
EFFECT: increased area of the spacecraft rollover stability during its landing.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
SPACECRAFT LANDING DEVICE | 2017 |
|
RU2675042C1 |
SPACE CRAFT LANDING DEVICE | 2017 |
|
RU2665154C1 |
SPACE VEHICLE LANDING DEVICE | 2012 |
|
RU2521451C2 |
SPACECRAFT LANDING SUPPORT DISCLOSURE SYSTEM | 2019 |
|
RU2725004C1 |
LANDING GEAR WITH CRUSH SUPPORTS FOR SPACECRAFT | 2014 |
|
RU2580601C1 |
SPACECRAFT LANDING GEAR | 2013 |
|
RU2546042C2 |
EXTENDABLE BOOM DEVICE | 2021 |
|
RU2772764C1 |
SPACECRAFT FOR DELIVERING PAYLOAD TO SPACE BODY WITH SMALL GRAVITATIONAL FIELD | 2020 |
|
RU2758656C1 |
MULTI-PURPOSE UNMANNED AIRCRAFT MISSILE SYSTEM | 2022 |
|
RU2791754C1 |
REUSABLE MODULAR TRANSATMOSPHERIC VEHICLE | 2022 |
|
RU2787063C1 |
Authors
Dates
2017-06-05—Published
2015-10-27—Filed