FIELD: rocketry. SUBSTANCE: proposed stand contains support element and thrust pickup connected to engine and to stop surface. Hinge device is installed between engine and stop surface, and support element is made in form of ring secured on engine at nozzle bottom and support frame square to longitudinal axis of engine connected with ring by flexible ties of adjustable length. EFFECT: reduced error at thrust measuring. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BENCH FOR STATIC TESTS OF ROCKET ENGINE HOUSING | 2008 |
|
RU2388926C1 |
| METHOD OF MEASUREMENT OF ROCKET ENGINE THRUST MOMENTUM AND TEST BENCH FOR ITS REALIZATION | 1994 |
|
RU2091736C1 |
| STAND FOR ACCELERATED SIMULATION TESTING OF WHEELED MACHINES UNDER FRAME PARTS | 1991 |
|
RU2019806C1 |
| RACK FOR MEASUREMENT OF AXIAL FORCE OF ROCKET ENGINE TRACTION | 2014 |
|
RU2554668C1 |
| METHOD AND DEVICES FOR TESTING SMALL ARMS AND/OR STAND TESTS OF ROCKET ENGINES | 2022 |
|
RU2790353C1 |
| LIQUID-PROPELLANT ROCKET ENGINE UNITS ATTACHMENT | 2014 |
|
RU2573628C2 |
| BENCH TO TEST SOLID-PROPELLANT ROCKET ENGINE "COCOON"-TYPE BODY FOR INTERNAL PRESSURE | 2014 |
|
RU2554695C1 |
| METHOD AND DEVICE FOR TESTING SMALL ARMS AND/OR BENCH TESTS OF ROCKET ENGINES | 2023 |
|
RU2799168C1 |
| MISSILE LAUNCHER WITH LASER-DRIVEN ROCKET ENGINE | 2016 |
|
RU2618558C1 |
| PENDULUM TEST STAND FOR ROCKET AND SMALL-ARMS WEAPON | 2003 |
|
RU2237844C1 |
