FIELD: rocketry. SUBSTANCE: method is based on change of pressure of gas medium in compartment relative to pressure on its surface through efflux of gas medium from compartment at action of aerodynamic flow. Change in pressure inside compartment is preliminarily determined by the flight trajectory. Efflux of gas medium is effected to local zone of surface at outside pressure equal to pressure inside compartment in mode of maximum pressure drops in the flight trajectory. In some versions, device have drainage holes whose positions are selected taking into account gradient of change of outside pressure in the flight trajectory; effective area is selected taking into account volume of compartment occupied by gas medium, flow coefficient of drainage hole and maximum drop of pressure between cavity of compartment and outside pressure. EFFECT: enhanced strength. 4 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF CONTROL OF AERODYNAMIC LOADS ACTING OF FLYING VEHICLE CASE AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) | 1999 |
|
RU2145564C1 |
FLYING VEHICLE COMPARTMENT | 1999 |
|
RU2164883C1 |
AFT BODY OF AIRCRAFT WITH ANNULAR LOCATION OF JET ENGINE NOZZLES ON ITS BOTTOM PROTECTION (VERSIONS) | 2013 |
|
RU2557125C2 |
METHOD OF DETERMINATION OF FLOW RATE CHARACTERISTICS OF DRAINAGE FACILITIES OF FLYING VEHICLE CASE AND SYSTEM FOR REALIZATION OF THIS METHOD | 2003 |
|
RU2267108C2 |
FLIGHT VEHICLE COMPARTMENT | 2008 |
|
RU2376198C1 |
AIRCRAFT COMPARTMENT | 2008 |
|
RU2374129C1 |
METHOD OF ESTIMATION OF UNTIGHTNESS OF FLYING VEHICLE COMPARTMENT PROVIDED WITH DRAINAGE DEVICES | 2003 |
|
RU2246708C1 |
METHOD FOR DETERMINATION OF FLOW-RATE CHARACTERISTICS OF DRAINAGE DEVICES OF FLIGHT VEHICLE COMPARTMENT AND SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2253095C2 |
THERMAL PROTECTIVE COATING OF HIGH-SPEED AIRCRAFT BODY | 2019 |
|
RU2719529C1 |
LOAD-BEARING PANEL OF SPACECRAFT SOLAR BATTERY (VERSIONS) | 2004 |
|
RU2283798C2 |
Authors
Dates
2000-02-20—Published
1999-06-25—Filed