FIELD: airpower.
SUBSTANCE: invention can be used to free up large-size power units that are detachable during operation and reusable, for example head shields, vehicle stages and compartments, external tanks of aircrafts, space vehicles and other disposable loads (DL). In the method of detaching disposable payload, the selection of spring pushers with different energies is used. Spring pushers with maximum and minimum energy are diametrically opposed to each other, determine the displacement of energy of pusher springs and the radius of displacement of pushers spring energy relative to the geometric center of mass. In order to avoid twisting of the DL relative to the longitudinal axis, the longitudinal pushers are alternately arranged with the right and left guiding.
EFFECT: securing the detaching of useful payloads with a given linear speed and eliminating the twisting of useful payloads relative to the longitudinal axis.
2 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR FORMING PAYLOAD SEPARATION SYSTEM | 2004 |
|
RU2293691C2 |
SYSTEM OF SEPARATION OF PAYLOAD OF SPHERICAL SHAPE | 2003 |
|
RU2276046C2 |
PAYLOAD SEPARATION SYSTEM | 2003 |
|
RU2268208C2 |
SEPARATION UNIT FOR SEVERAL LOADS PAYLOADS FROM A SINGLE LAUNCH VEHICLE | 2018 |
|
RU2680468C1 |
PAYLOAD SEPARATION SYSTEM | 2005 |
|
RU2293694C1 |
PAYLOAD SEPARATION SYSTEM | 2009 |
|
RU2396191C1 |
WORKING LOAD SEPARATION DEVICE | 2015 |
|
RU2648522C2 |
MASTER DEVICE WITH TORSION SPRINGS | 2006 |
|
RU2333455C2 |
SYSTEM FOR SEPARATING PAYLOAD FROM SPACE VEHICLE BOARD | 2011 |
|
RU2471684C1 |
TURNTABLE FOR SECURING PAYLOAD | 2003 |
|
RU2238888C1 |
Authors
Dates
2018-01-09—Published
2016-03-24—Filed