FIELD: astronautics.
SUBSTANCE: group of inventions relates to the aerospace equipment. Transfer compartment contains hull with spacer. Hull contains docking and supporting frame. In the cross-section the docking frame is made in the form of T-shaped profile with the bent inside the compartment wall. Spacer comprises connected to the payload upper frame, fixed to the hull supporting frame lower frame, and arranged along the spacer upper end and connected to each other by arcs brackets. Hull docking frame and the spacer upper frame are connected to the triangular grid by the flat truss. In the cross-section supporting frame is made in the form of double tee-shaped profile with transverse ribs located in the open to the frame outside circular niche. In the frame bottom flange between the transverse ribs through holes are made. In the frame upper flanges, the holes are made blind and arranged above the transverse ribs. In the frame upper flange middle part the spacer lower frame is fixed. On the supporting frame upper flange outer arm peripheral part the hull longitudinal beams and shell are fixed. Frame lower flange is connected to the carrier rocket.
EFFECT: technical result is the transfer compartment weight reduction and increase in the carrying capacity.
15 cl, 30 dwg
Title | Year | Author | Number |
---|---|---|---|
CARRIER ROCKET TRANSIENT COMPARTMENT AND TRUSS | 2018 |
|
RU2697493C1 |
TRANSFER COMPARTMENT OF CARRIER ROCKET (VERSIONS) | 2015 |
|
RU2603872C1 |
FORMER | 2018 |
|
RU2694486C1 |
ROCKET BOOSTER | 2009 |
|
RU2412871C1 |
ASCENT UNIT | 2014 |
|
RU2564458C1 |
TRANSFER COMPARTMENT OF SPACE MISSION VEHICLE ASSEMBLY-PROTECTIVE UNIT | 2013 |
|
RU2521078C1 |
DOUBLE START SYSTEM AND SUPPORT ASSEMBLY | 2018 |
|
RU2694487C1 |
METHOD OF SPACESHIP SPACECRAFT NOSE CONE ASSEMBLY AND DEVICE TO THIS END | 2014 |
|
RU2560963C1 |
TRANSITIONAL TRUSS | 2021 |
|
RU2779010C1 |
SPACE ROCKET SYSTEM | 2007 |
|
RU2349512C1 |
Authors
Dates
2018-07-17—Published
2017-09-04—Filed