FIELD: rocketry. SUBSTANCE: the antiaircraft missile consists of a sustainer stage, whose body shell is joined to the nose fairing, functional units, staging mechanism and a zero stage. Part of the functional units is made in the form of weight simulators of control actuator units with control surfaces installed on the frames in succession one after another, and a warhead in the form of a steel tube with a made thread and weights radially positioned on it. The rest part of the functional units incorporates a power unit with an inertia switch and a flare. The control surfaces of the control actuator are installed in parallel with the missile longitudinal axis and locked, and the weights of the warhead simulator are installed for movement on the tube. EFFECT: provision of determination of the missile ballistic characteristic and its dispersion at firing to a simulated point in the stage of development work. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTIAIRCRAFT GUIDED ROCKET | 2001 |
|
RU2191986C1 |
ANTIAIRCRAFT GUIDED MISSILE | 1998 |
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ANTI-AIRCRAFT TARGET MISSILE | 1998 |
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GUIDED ANTI-AIRCRAFT MISSILE | 2002 |
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GUIDED ANTI-AIRCRAFT MISSILE | 2000 |
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GUIDED ANTI-AIRCRAFT MISSILE | 2000 |
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TWO-STAGE GUIDED MISSILE | 2007 |
|
RU2357201C2 |
GUIDED MISSILE | 2004 |
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RU2258898C1 |
ANTI-AIRCRAFT TARGET MISSILE | 2002 |
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RU2222767C1 |
RADIO-CONTROLLED ANTI-AIRCRAFT MISSILE | 2000 |
|
RU2189003C2 |
Authors
Dates
2001-06-20—Published
1999-12-06—Filed