FIELD: astronautics.
SUBSTANCE: group of inventions relates to space engineering. Power unit of the reusable vehicle contains rocket engine (4) mounted on cradle (2). Cradle (2) comprises at least three fastening elements (9) for connecting said unit to the structure of the carrier apparatus. At least three fastening elements form dismounting plane (12) of the unit, the unit comprising one or more hydraulic and/or electrical connections of said motor (4), each of these connections comprising free end (11) intended to be connected to a suitable power system of the carrier apparatus on which the power unit is to be installed, wherein the end of at least some of said free ends (11) is in said dismounting plane (12). Rigging device for mounting/dismounting and transporting the power unit comprises two longitudinal guides (14, 17) fixedly connected to mobile frame (13), movable carriage (18) with two pairs of removable supporting pillars (19), which is translatable along guides (14, 17).
EFFECT: technical result of the group of inventions is the simplification of the design of the power unit and the operations of its installation and dismantling.
25 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF SERVICING COSMIC ARTICLES AND SHUTTLE AEROSPACE SYSTEM FOR ITS IMPLEMENTATION | 2007 |
|
RU2342288C1 |
DEVICE FOR RETAINING TANK IN AIRCRAFT | 2014 |
|
RU2662588C2 |
AEROSPACE AIRCRAFT | 2010 |
|
RU2436715C2 |
AQUA AEROSPACE VEHICLE | 2012 |
|
RU2626418C2 |
METHOD OF INJECTION OF PAYLOAD INTO NEAR-EARTH SPACE BY MEANS OF AIRCRAFT ROCKET SPACE COMPLEX AND AIRCRAFT ROCKET SPACE COMPLEX FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2265558C1 |
AIRCRAFT (VERSIONS), TAKEOFF-LANDING GEAR (VERSIONS) AND METHOD OF LIFTING AIRCRAFT IN AIR (VERSIONS) | 2012 |
|
RU2588198C2 |
PAYLOAD LAUNCHING AND TRANSPORTATION SYSTEM | 1999 |
|
RU2233772C2 |
METHOD OF INJECTION OF OBJECTS INTO NEAR-EARTH ORBIT AND RECOVERABLE AERO-SPACE ROCKET AIRCRAFT-CARRIER FOR REALIZATION OF THIS METHOD (AERO-SPACE SYSTEM NUR-SAID SYSTEM) | 2001 |
|
RU2232700C2 |
MOBILE LAUNCHER UNIT | 2020 |
|
RU2739477C1 |
HIGH-SPEED TRANSPORT SYSTEM, ROTOR-CYLINDER ENGINE, RECOVERABLE GROUND AIR AND RECOVERABLE WATER-AND-AIR SPACE SYSTEMS | 2001 |
|
RU2217358C2 |
Authors
Dates
2018-06-28—Published
2014-07-04—Filed