FIELD: military equipment.
SUBSTANCE: invention relates to transport and launch containers (TLC), and is intended for storage, transportation and launch of missiles with the possibility of uneven heating. TLC is made in the form of a cylindrical multilayer thin-walled shell of a composite material. It contains top and bottom covers with seals. A carbon fibre thread is wound between the layers of the shell along its entire length and current leads made of a metal tape are installed. The winding of the carbon fibre thread is made unevenly along the helix, while the turns of the thread are not adjacent to each other.
EFFECT: possibility of uneven heating of the rocket in the TLC is achieved.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AUTOMATIC LOADING SYSTEM OF ROCKETS IN SELF-PROPELLED LAUNCHING VEHICLE | 2014 |
|
RU2578917C1 |
| LAUNCHER MISSILE FIXING UNIVERSAL MODULE | 2015 |
|
RU2613205C2 |
| MULTILAYERED HOUSING OF TRASNPORT-LAUNCHER CONTAINER FROM COMPOSITE MATERIALS (VERSIONS) | 2012 |
|
RU2507469C2 |
| LAUNCH DEVICE | 2022 |
|
RU2787533C1 |
| DEVICE FOR POSITIONING TRANSPORT-LAUNCHING CONTAINER ON LAUNCHER | 2010 |
|
RU2432543C1 |
| STARTING DEVICE | 2022 |
|
RU2801754C1 |
| TRANSPORTER-LAUNCHER CONTAINER | 2007 |
|
RU2350885C1 |
| TRANSPORT AND LAUNCH MODULE | 2020 |
|
RU2754025C1 |
| LAUNCHER | 2006 |
|
RU2309362C1 |
| METHOD OF MAKING HOUSING OF TRANSPORT-LAUNCH CONTAINER OF COMPOSITE MATERIALS (VERSIONS) | 2011 |
|
RU2492048C1 |
