我参与的买进瓦良格的艰难历程及幕后故事(ZT)

Catamaran

致敬

xiaoriver

金牛银熊

Specifications
		Mod-1		Mod-2		Mod-3
DIA		SS-20		SS-20		SS-20/SS-X-28
NATO		Saber		Saber		Saber
Bilateral		RSD-10		RSD-10		RSD-10
Service		RSD-10/Pioneer		RSD-10/Pioneer-UTTX		RSD-10/Pioneer-3
OKB/Industry		15Zh45 (Temp-2C)		15Zh53 (Temp-2C)		15Zh53 (Temp-2C)
Design Bureau		Moscow Institute of Thermal Technology		Moscow Institute of Thermal Technology		Moscow Institute of Thermal Technology
Approved		3/4/1968		7/19/1977		8/14/1980
Years of R&D
Engineering and Testing		1974-76		1974-1976		1979-1980
First Flight Test		9/21/74		9/21/74		8/10/1979
IOC		1976		1976		1980
Deployment Date		3/11/1976		3/11/1976		12/17/1980
Type of Warhead		Single		MIRV		Single or MIRV
Warheads		1		3		1/3
Yield (Mt)		1.0		0.15		?
Payload (t)		1.5-1.74		1.5-1.74		?
Total length (m)		16.49		16.5		17.0
Total length w/o warhead (m)		14.9		14.9		14.9
Missile Diameter (m)		1.79		1.79		1.79
Launch Weight (t)		37		37		37
Fuel Weight (t)
Range (km)		600-5000		600-5000		600-5500/7500
CEP (m) Russian Sources		0.550		0.550		0.450
CEP (m) Western Sources		150-450		400-430`		?

Number of Stages		2
Canister length (m)		19.32
Canister length w/o front (m)
Canister diameter (m)		2.14
Booster guidance system		Inertial, autonomous

		1st stage		2nd stage	2nd Stage
Length (m)		8.58		4.4-4.6	4.4-4.6
Body diameter (m)		1.79		1.47	1.47
Fueled weight (t)		26.7		8.63	8.63
Dry weight (t)
Solid Motor Designation
Design Bureau
Years R & D
Propellants		Solid		Solid	Solid
Fuel		N/A		N/A	N/A
Oxidizer		N/A		N/A	N/A
Burning time (sec.)		63
Thrust Sea Level/Vacuum (Tonnes)
Special Impulse (sec.)

Basing Mode		Ground mobile
Hardness
Launching Technique		Mortar Launch
Deployed boosters		0
Test Boosters
Warheads Deployed		0
Deployment Sites		INF Treaty data
Training Launchers
Space Booster Variant		N/A

Yiso

happylux

原帖由 金牛银熊 于 2009-1-20 07:11 PM 发表 苏联帝国，在苏联总统戈尔巴乔夫的新思维运动推动下，轰然倒塌了。这个在近代史上数度鲸吞我国领土和多年与我为敌的庞然大物，出乎几乎所有世人的意料，一夜之间竟然迅速分崩离析了！几十年来，在数千公里边境 ...

This is insteresting, post more.

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