FIELD: flying vehicles. SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening to chambers and vehicle body to provide turning of vehicle. Each chamber is connected with two neighbor chambers by tie-rods with end joints. Both joints can be made ball-type, or one of joints is ball-type, and the other is one-axis joint. Lengths between centers of joint tie-rods are equal to each other are parallel to lengths between centers of hangers of connected chambers. Number of actuators is equal to number of chamber. So one actuator with ball joint and/or one-axis joint belongs to each actuator. EFFECT: reduced size of power plant in diameter. 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROLLABLE LIQUID-PROPELLANT MULTI-CHAMBER ROCKET VEHICLE | 1999 |
|
RU2156874C1 |
| ENGINE FOR LIQUID-PROPELLANT ROCKET POWER PLANT | 1996 |
|
RU2119081C1 |
| AIRCRAFT ENGINE UNIT | 1995 |
|
RU2089743C1 |
| HINGED SUSPENSION FOR MOUNTING REACTION CHAMBER ON FLYING VEHICLE | 1995 |
|
RU2090773C1 |
| ANNULAR JET NOZZLE OF VARIABLE GEOMETRY | 1999 |
|
RU2150600C1 |
| MULTISTAGE ROCKET | 1994 |
|
RU2088787C1 |
| METHOD OF STARTING LIQUID ROCKET ENGINE AND LIQUID ROCKET ENGINE | 1994 |
|
RU2084677C1 |
| METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT | 2001 |
|
RU2209993C2 |
| THROTTLEABLE OXYGEN-HYDROCARBON LIQUID-PROPELLANT ROCKET ENGINE WITH AFTERBURNING OF RECOVERY GAS | 2002 |
|
RU2238423C2 |
| METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE AT TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT | 1999 |
|
RU2166661C1 |
