FIELD: aircraft engineering.
SUBSTANCE: invention relates to rocketry, particularly, to rockets in transport-and-launch container to be installed at sips, submarines and ground stationary and moving launchers. Rocket (1) is arranged in transport-and-launch container (2) with cylindrical part (3) and conical part (4) of guide surface. Thrust surfaces of the rocket cruising stage front part elements are composed of an integral conical surface with tape angle that allows a maximum length of contact between rocket conical thrust surface and conical guide surface of transport-and-launch container front part.
EFFECT: reduced loads and in-flight drag, increased rocket midsection.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LAUNCHER FOR MULTI-BELT-REST MISSILES | 2012 |
|
RU2494334C1 |
| CRUISING MISSILE IN TRANSPORTATION-LAUNCHING CONTAINER | 2001 |
|
RU2215981C2 |
| METHOD AND DEVICE FOR GUIDED MISSILE TAKE-OFF FROM TRANSPORT-LAUNCHING PACK | 2003 |
|
RU2240489C1 |
| UNDERWATER MISSILE | 2007 |
|
RU2352894C1 |
| TRANSPORTER-LAUNCHER CONTAINER | 2007 |
|
RU2350885C1 |
| MODULAR MULTI-SEAT SHIPBOARD LAUNCHER OF VERTICAL LAUNCH | 2008 |
|
RU2393409C1 |
| SELF-PROPELLED LAUNCHER | 2008 |
|
RU2386918C1 |
| SUPERSONIC MISSILE | 2017 |
|
RU2686567C2 |
| MULTIFUNCTIONAL SMALL-SCALE TRANSFORMABLE REUSABLE UNMANNED AERIAL VEHICLE IN TRANSPORT-LAUNCH CONTAINER AND STARTING METHODS | 2022 |
|
RU2778177C1 |
| METHOD OF MISSILE MOVEMENT STABILIZATION AT UNDERWATER LAUNCH AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2607126C1 |
