FIELD: rocketry, in particular, overheat protection of missile body.
SUBSTANCE: at the outlet from the gas source that is positioned in the missile body, the passage is divided in the point of branching. Installed in the body is a cylinder with a double-acting piston and a rod kinematically linked with the switch. Inlets are made on the opposite ends of the cylinder, each of them is connected to one of the hoses, and made between the inlets in the cylinder is a outlet communicating with the holes in the missile body through a cavity formed between the cylinder and the body.
EFFECT: enhanced efficiency of overheat protection of the supersonic missile body.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AERODYNAMIC UNIT OF STEERING GEAR OF GUIDED MISSILE | 2002 |
|
RU2206058C1 |
| ROCKET | 2000 |
|
RU2183816C2 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2000 |
|
RU2172927C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 1999 |
|
RU2151317C1 |
| PRESSURE RATIO PICKUP | 0 |
|
SU857765A1 |
| GUIDED MISSILE | 2004 |
|
RU2247311C1 |
| GAS DYNAMIC IGNITER | 2011 |
|
RU2485402C1 |
| FLYING VEHICLE AIR INTAKE | 2005 |
|
RU2287456C1 |
| POWER PLANTS WITH IMPROVED CRANKCASE GAS EXHAUST, GAS EXHAUST AND DUST REMOVAL PROCESSES, REDUCING THE INFRARED SIGNIFICANCE OF A MILITARY TRACKED VEHICLE | 2023 |
|
RU2802967C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 1999 |
|
RU2148726C1 |
