FIELD: measurement of forces. SUBSTANCE: invention is specifically related to benches for firing tests of engines of flying vehicles. It is aimed at provision of conditions of starting of power plant approximate to operational conditions, at separated functioning of its units, at change of time of delay of initiation of firing of solid fuel pressure accumulator and at investigation of effect of time delay on intraballistic characteristics of sustainer engine and solid fuel pressure accumulator. Specific feature of invention lies in division of bearing unit of plant into mobile and immobile subunits. Mobile subunit is manufactured in the form of parallelogram suspension with adjusted moment of inertia and is fitted with arm locking extreme position. EFFECT: provision of starting conditions close to operational conditions. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET STAGE JOINT | 2001 |
|
RU2196956C1 |
ROCKET | 2005 |
|
RU2293283C1 |
SYSTEM OF ROCKET LAUNCHING FROM LAUNCH CONTAINER | 2009 |
|
RU2400688C1 |
ROCKET | 1998 |
|
RU2134860C1 |
JET ENGINE IGNITION DEVICE | 1997 |
|
RU2127821C1 |
SOLID-PROPELLANT ROCKET ENGINE | 1998 |
|
RU2153093C1 |
PROPULSION INSTALLATION | 2010 |
|
RU2428580C1 |
SOLID-PROPELLANT ROCKET ENGINE | 1996 |
|
RU2118686C1 |
SOLID-FUEL ROCKET ENGINE | 1997 |
|
RU2134814C1 |
SOLID-PROPELLANT ROCKET ENGINE | 1996 |
|
RU2109160C1 |
Authors
Dates
2000-09-27—Published
1999-07-27—Filed