System
Name
[US
name]#
Range and Payload
Warhead
and
YieldPropulsion
and
GuidanceEst.
CEPComment
DF-2
[CSS-1]0 1.9-3.7 km No longer deployed DF-3/3A
[CSS-2]40 2850 km 2150 kg
-Single nuclear warhead,
1-5 MT
(3.3 MT)-Single conv. warhead
Single-stage; storable liquid propellant (AK-27/UDMH); Fully inertial strap-down guidance system 2.5-4.0 km 120-150 minute launch prep. time; road-mobile; all DF-3 scheduled to be replaced by the DF-21 DF-4
[CSS-3]20 4850-5500 km 2200 kg
Single nuclear warhead,
1-5 MT
(3.3 MT)Two-stage, non-storable liquid propellant (LOX/
kerosene)3.0-3.5 km 60-120 minute launch prep. time; also used as booster for CZ-1 SLV; cave-based and rolled out to launch DF-5/5A
[CSS-4]18-26 13000+
km3200 kg
Single nuclear warhead,
1-5 MT
(4-5 MT)Two-stage; storable
liquid propellant (N2O4/
UDMH); gyro-platform with onboard computer0.5-3.0 km 30-60 minute launch prep. time; also used as booster for CZ-2, CZ-3, CZ-4 SLVs; deployed at silos at 3 locations DF-21/21A
[CSS-5]
[Mod 1&2]48 1800
km600 kg
-Single nuclear warhead, 200-300 kT -Single conv. warhead
Two-stage; solid propellant;
gyro-platform inertial guidance with onboard computer; working on
terminal guidance system0.3-0.4 km 10-15 minute launch prep. time; land-mobile; reportedly replacing DF-3 in some areas; same missile as JL-1 SLBM; longer range Mod 2 to replace Mod 1 by 2005 DF-15/M-9
[CSS-6/
CSST-600]8-50? 600 km
950 kg
-Single nuclear warhead, 50-350 kT -Single or cluster conv. warhead
Single-stage;
solid propellant;
strap-
down inertial computer-digitized
guidance system with terminal control600 m 30 minute launch prep. time; M-9 version designed explicitly for export; the nuclear role for the CSS-6 is as yet unproven; enhancing accuracy with GPS tech. DF-11/M-11
[CSS-X-7]200? 300 km
800 kg
-Single nuclear warhead, 350 kT -Single or cluster conv. warhead
Two-
stage;
solid propellant;
strap-
down inertial computer-digitized guidance system with terminal control150 m 30-45 minute launch
prep. time; M-11 version designed explicitly
for exportM-7/8610
[CSS-8]? 160 km 190 kg
Conv.
warheadTwo-stage; solid propellant booster and storable liquid propellant main engine Modification of HQ-2 (SA-2) SAM; mobile DF-25
(possibly cancelled)0 1700 km 2000
kg-Single conv. warhead Two-stage; solid propellant Development cancelled; based on first two stages of DF-31; land-mobile DF-31
(under
devt;
tested)0 8000 km 700
kg-Single nuclear warhead, 200-300 kT (100-200 kT) (500 kT) -Possible future
use with MRV/MIRV
capabilityThree-stage; solid propellant 0.5 km In late stages of devt.; tested on 8/2/1999; 10-15 minute launch prep. time; land-mobile; most likely cave-based; same missile as JL-2 SLBM; nuclear warhead awaits certification; to be operational around 2000; to replace the DF-4; could incorporate penetration aids such as decoys or chaff DF-41
(under
devt. not flight
tested)0 12000 km 800 kg (700 kg)
-Single nuclear warhead, 200-300 kT -Possibly equipped
with MRV/MIRV
capabilityThree-stage; solid propellant 0.7-0.8 km Under devt.; 3-5 minute launch prep. time; land-mobile; will replace DF-5; possible deployment around 2010; warhead awaits certification; may be cancelled and replaced by a new solid-propellent, mobile ICBM that is currently in development JL-1
[CSS-N-4]
SLBM12 1700 km 600 kg
-Nuclear warhead, 200-300 kT (500 kT) Two-stage; solid propellant;
gyro-platform inertial guidance with onboard computer1.0 km Same missile as the DF-21/21A JL-2
[CSS-N-5]
SLBM
(under
devt.,
not yet tested)0 8000 km 700 kg
-Nuclear warhead, 200-300 kT -Possibly will be equipped with MRV/MIRV
capabilityThree-stage; solid propellant 1.0 km Under devt.; same missile as the DF-31; projected to be operational around 2003; warhead awaits certification. To be deployed on new 09-4 SSBN which is currently under devt.; 09-4 will likely be deployed by 2010 DF" stands for "Dong Feng" ("East Wind")
"JL" stands for "Julang" ("Great Wave")
"CSS" stands for "Chinese Surface-to-Surface"
"CSS-N" stands for "Chinese Surface-to-Surface Naval"
"CSST" stands for "Chinese Surface-to-Surface Tactical"
Wednesday, 29 October 2008
Chinese Ballistic Missile Designation and Characteristics
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