| Specifications |
| Contractor |
|
| Initial operational capability |
1961 |
| First detected |
1961 |
| Production terminated |
1965 |
| Type |
long-range anti-ship standoff missile |
| Wingspan |
4.6-4.88 m |
| Length |
9.5 m |
| Diameter |
0.9 m |
| Launch weight |
4200 kg |
| Max. speed |
1400 km/h |
| Ceiling |
12000 m |
| Maximum range |
260-350 km |
| Propulsion |
Lyulka AL-5 RD-9FK liquid fuel turbojet |
| Guidance |
active radar homing |
| Warhead |
impact with delay-fuzed high explosive, 1000 kg or
nuclear 1000-kg warhead |
| Probability of hitting the target |
0.624 (during tests, according to the military, except for launches with equipment failures)
0.714 (during tests, according to the design bureau, except for unsuccessful launches with design flaws)
0.8 (according to the results of tests and training use in 1961, a figure agreed by the military and design bureau)
0.65 (from the number of successful launches, based on the results of the work of combat units, until 1963)
1.00 (from the number of successful launches, based on the results of the work of combat units, 1963)
0.87 (from the number of successful launches, based on the results of the work of combat units, 1964)
|
| Carrier aircraft |
Tu-16K-10
Tu-16K-10D
Tu-16K-10N
Tu-16K-10-26
Tu-95K-10 (draft)
Tu-22K-10 (draft)
| Variants |
K-10 - design version of the rocket;
K-10S - serial missile;
P-40 - anti-ship projectile for arming the nuclear cruiser pr. 63 (draft);
K-10P - a missile with a range increased to 300 km and a speed of 2700-3000 km / h, for arming the Tu-22K-10 (draft);
K-10SD - a missile with an increased flight range and a lighter warhead. Additional fuel tank for 200 l. fuel in the guidance equipment compartment;
K-10SN - low-altitude modification for the Tu-16K-10N carrier, R&D apparently began in 1961. The possibility of launching from an altitude of 500-600 m was laid down. The stabilized flight altitude at the active guidance stage decreased from 1200 to 600 m, the flight altitude at the final stage is 90-150 m. The complex was put into service.
K-10SP - a modification of the K-10SN developed in 1972-1979, equipped with the Azalia active jamming station and designed to cover the launch of combat missiles. The missile carriers equipped for the use of these missiles were designated as Tu-16K-10P, and the complex as a whole received the designation K-10P
K-10SDV - an improved low-altitude missile with an increased range, a modified guidance and control system; The complex was adopted.
K-10M - target missile for naval air defense training, development was carried out between 1959 and 1961. R&D was discontinued.
K-14 - a variant of the missile for Myasishchev's long-range missile carriers (project) Start of R&D - August 1959, termination of R&D - February 5, 1960
|
