FIELD: transport.
SUBSTANCE: invention relates to launching systems for, mainly, carrier rockets. Proposed method consists in using artillery barrel arranged vertically in water reservoir with its top end kept afloat by pontoons. Note here that initial acceleration of the rocket mounted at barrel bottom on piston is generated by hydrostatic pressure on said piston from below. Besides, powder charge arranged between the piston and charged rocket is ignited to suppress shot recoil via reservoir liquid. Proposed device comprises elements and units required to implement proposed method, e.g. for forcing water from the barrel, mounting the rocket and forcing water under the piston.
EFFECT: application of hydrostatic pressure accumulated in water reservoirs and their damping ability, as well as powder combustion power that allow notable increase in take-off mass.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LAUNCHING COMPLEX AND METHOD FOR LAUNCHING CARRIER ROCKETS WITHOUT USING THE FIRST STAGE | 2020 |
|
RU2733449C1 |
| METHOD OF BLASTING HIGH-POWER AMMUNITION AND AMMUNITION TO THIS END | 2007 |
|
RU2399864C2 |
| METHOD OF ROCKET SHOT FIRING AND ROCKET SHOT FOR ITS REALIZATION | 1993 |
|
RU2082930C1 |
| METHOD OF SINGLE IMPACT TEST OF OBJECT | 2004 |
|
RU2267107C2 |
| METHOD FOR PROTECTION OF TERRITORIAL WATERS AND DEVICE FOR ITS REALISATION | 2007 |
|
RU2397431C2 |
| METHOD TO FACILITE ICE STARTING AT LOWER TEMPERATURES AND DEVICE TO THIS END | 2006 |
|
RU2373423C2 |
| ORBITAL INJECTION SYSTEM | 1994 |
|
RU2077017C1 |
| GLIDING AMMUNITION | 2012 |
|
RU2509287C1 |
| METHOD AND DEVICE FOR COMPONENT MECHANICAL TESTS | 2010 |
|
RU2442122C1 |
| BENCH FOR SHOCK-TESTING | 2002 |
|
RU2235302C2 |
