RU96113157A - SUPERSONIC CONTROLLED ROCKET - Google Patents
SUPERSONIC CONTROLLED ROCKETInfo
- Publication number
- RU96113157A RU96113157A RU96113157/02A RU96113157A RU96113157A RU 96113157 A RU96113157 A RU 96113157A RU 96113157/02 A RU96113157/02 A RU 96113157/02A RU 96113157 A RU96113157 A RU 96113157A RU 96113157 A RU96113157 A RU 96113157A
- Authority
- RU
- Russia
- Prior art keywords
- supersonic
- rocket
- controlled rocket
- controlled
- rudders
- Prior art date
Links
Claims (1)
где Sр - площадь руля:
Sкр - площадь крыла;
Gp - вес ракеты;
Gб - вес боевой части.A supersonic guided missile containing a head, a cylindrical body, rudders and wings, characterized in that the rudders and wings are made with areas according to the ratio
where S p - rudder area:
S cr - wing area;
G p - rocket weight;
G b - the weight of the warhead.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96113157A RU2114384C1 (en) | 1996-06-21 | 1996-06-21 | Supersonic guided missile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96113157A RU2114384C1 (en) | 1996-06-21 | 1996-06-21 | Supersonic guided missile |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2114384C1 RU2114384C1 (en) | 1998-06-27 |
RU96113157A true RU96113157A (en) | 1998-09-10 |
Family
ID=20182585
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96113157A RU2114384C1 (en) | 1996-06-21 | 1996-06-21 | Supersonic guided missile |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2114384C1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103115532B (en) * | 2013-03-05 | 2014-11-05 | 西北工业大学 | Supersonic missile anti-drag wings |
RU2668633C1 (en) * | 2017-05-17 | 2018-10-02 | Крутяков Ювеналий Александрович | Device for achieving supersonic speeds of low mass shells |
-
1996
- 1996-06-21 RU RU96113157A patent/RU2114384C1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69401901D1 (en) | Ammunition with projectiles connected by ropes | |
DE69106913D1 (en) | Torpedo warhead with hollow and explosive charge. | |
RU96113157A (en) | SUPERSONIC CONTROLLED ROCKET | |
JPS63500328A (en) | inertial guided missile | |
KR970705000A (en) | Training projectiles | |
KR910012652A (en) | Adjustable spacer in warhead with hollow grasping | |
FR2702553B1 (en) | Telescoped type ammunition. | |
DE3264956D1 (en) | Hair-roller and its application to forming hair | |
CA2183279A1 (en) | Missile Having Non-Cylindrical Propulsion Section | |
NO150820C (en) | WINGHOUSE CONSTRUCTION FOR SELF-RISING WINGS IN PROJECTILES, ROCKETS AND SIMILAR | |
NO872320D0 (en) | Projectile body. | |
RU93026507A (en) | ROCKET HEAD | |
RU97105048A (en) | ROCKET-CARRIER-RING | |
GB2072309A (en) | Small arms ammunition | |
Oberle et al. | The Application of Electrothermal-Chemical(ETC) Propulsion Concepts to Reduce Propelling Charge Temperature Sensitivity | |
RU2002131042A (en) | ROCKET | |
EP0987513A3 (en) | Subcalibre projectile | |
RU2004121005A (en) | ROCKET | |
JPS6438498U (en) | ||
DE3376451D1 (en) | Training projectile | |
SU1692243A1 (en) | Anti-hail rocket | |
IT1183971B (en) | Telescoping head for bombs, rockets and missiles | |
RU94005577A (en) | ARTILLERY SHELL | |
ZA866867B (en) | Launching missiles,missile launcher,missile and controlling rioters | |
ATE76500T1 (en) | IGNITION DEVICE, IN PARTICULAR FOR A PROPULSION CHARGE OF A RECOILESSLESS ANTI-TANK PRACTICE WEAPON. |