DF-15 (missile)
| DF-15 | |
|---|---|
| Kind | SRBM |
| The operational history | |
| Deployment | |
| History of development | |
| Manufacturer | Academy of Rocket Motors Technology |
| Specifications | |
| Weight | 6,200 kg |
| Full length | 9.1m |
| Diameter | 1.0m |
| | |
| Warhead | One plane and movement possibility type re-entry body [1] |
| The nuclear output | 350-500kT |
| | |
| Engine | One step-type solid rocket |
| Instruction method | Inertial guidance+GPS, Fixed star astronomical navigation+Ring laser gyroscope |
A short-range ballistic missile (SRBM) that China developed DF-15 (average: easterly wind -15, Dong-Feng-15, an export name: M-9, DoD cord: CSS-6). It is managed in a second gunner corps of People's Liberation Army.
Table of contents
Summary
Development began in 1985, and a design was approved in 1987, and a discharge experiment was conducted in the Gobi in the 1980-1990 generation. By the guess of the American Department of Defense of 2009, they increase more than 100 a year, and, as for the number of the deployment, 350-400, the discharge radix are done with 90-110 engines [2]. Taiwan is aimed for, and the most are deployed in Fujian [2].
The missile transportation and a discharge vehicle is eight drive cars of TA5450 or WS2400. I move to an emergency using a railroad from the base and shoot it. The support people under the equipment corps servant present a smoke screen and prevent the cover discovery with a reconnaissance satellite and the spy plane.
It can be launched from the development of the missile and, at time, is quite said to be 15-30 minutes.
Specifications
- Range = 600km
- Warhead = 1
- Warhead power = 350-500kT
- Engine = single step-type solid rocket
- Instruction system = inertial guidance +GPS
- CEP= 150-500m
- Maximum velocity =
- Full length = 9.1m
- Diameter = 1.0m
- Weight = 6,200 kg
- Payload = 500 kg
- Production = Academy of Rocket Motors Technology
- Cost =
Explanatory note
Outside link
This article is taken from the Japanese Wikipedia DF-15 (missile)
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