SUPERSONIC GUIDED MISSILE Russian patent published in 1998 - IPC

Abstract RU 2114384 C1

FIELD: rocketry. SUBSTANCE: supersonic guided missile, whose control surfaces and wings have areas in relation: Sp/Swi=(0.11 to 0.14)ϕгp, 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

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RU 2 114 384 C1

Authors

Kuznetsov V.M.

Komissarenko A.I.

Maksimov F.A.

Dates

1998-06-27Published

1996-06-21Filed