FIELD: rocketry. SUBSTANCE: supersonic guided missile, whose control surfaces and wings have areas in relation: Sp/Swi=(0.11 to 0.14)ϕг/ϕp, where: Sp - control surface area; Swi - wing area; ϕp - missile mass (less propellant); ϕг - nose cone mass. EFFECT: enhanced developed g-load due to optimum selection of areas of aerodynamic controls and stabilization of wings. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
TWO-STAGE GUIDED MISSILE | 2007 |
|
RU2357201C2 |
ROCKET | 1995 |
|
RU2085826C1 |
ROCKET | 1996 |
|
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METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 |
|
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METHOD OF GUIDED MISSILE LAUNCHING AND DEVICE FOR ITS REALIZATION | 1997 |
|
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GUIDED MISSILE | 1998 |
|
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MISSILE | 2002 |
|
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GUIDED MISSILE | 1998 |
|
RU2135946C1 |
METHOD FOR FIRING OF GUIDED MISSILE WITH SEPARATING STAGES AND MISSILE COMPLEX FOR ITS REALIZATION | 1998 |
|
RU2148777C1 |
CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
Authors
Dates
1998-06-27—Published
1996-06-21—Filed