FIELD: rocket suspension and forced separation systems. SUBSTANCE: device has load-bearing housing where rocket forced separation mechanism, rocket holding mechanism, onboard connector mechanism and electric automatic control units are arranged. Rocket forced separation drive includes tactical pneumatic drive and one-time pyrotechnic drive connected by means of working lines. In the upper portion of housing there are wells for ejection device suspension units; free wells are closed with covers. Load-bearing housing is detachable and is rectangular in section; it is provided with side semicylindrical fairings. Its front portion is closed with fairing having arched section of double curvature; tail section is closed by fairing of conical-cylindrical shape with opening doors. Height of housing is equal to half diameter of rocket and width is about 0.3 of rocket calibre. EFFECT: improved aerodynamic characteristics of ejection device; enhanced reliability of holding the rocket. 3 cl, 7 dwg
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Authors
Dates
2000-02-20—Published
1999-06-10—Filed