503 lines
16 KiB
Plaintext
503 lines
16 KiB
Plaintext
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# ****************************************************************************
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# CUI
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#
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# The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
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#
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# The use, dissemination or disclosure of data in this file is subject to
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# limitation or restriction. See accompanying README and LICENSE for details.
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# ****************************************************************************
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# This model was derived from unclassified sources
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/* BEGIN COMMENT
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http://www.sinodefence.com/strategic/missile/df21.asp
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Specifications
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Official name: DongFeng 21 (DF-21)
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NATO reporting name: CSS-5
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Contractor: CASIC 4th Academy
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Service status: In service
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Configuration: Two-stage, solid propellant
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Deployment: Road mobile, 6X6 tractor truck + six-wheel trailer; or silo
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Length: 10.7m
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Diameter: 1.4m
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Launch weight: 14,700kg
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Range: 1,770km
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Re-entry vehicle mass: 600kg
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Warhead: One single 500kT yield, or conventional
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Guidance: Inertial + terminal radar guidance
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Accuracy: CEP 300~400m
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http://www.missilethreat.com/missilesoftheworld/id.26/missile_detail.asp
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CSS-5
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Country: People's Republic of China
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Alternate Name: DF-21
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Class: MRBM
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Basing: Road mobile
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Length: 10.70 m
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Diameter: 1.40 m
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Launch Weight: 14700 kg
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Payload: Single warhead, 600 kg
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Warhead: Nuclear 250 or 500kT, HE, submunitions, or chemical
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Propulsion: 2-stage solid
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Range: 2150 km
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Status: Operational
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In Service: 1987
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http://www.fas.org/nuke/guide/china/theater/df-21.htm
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Contractor Academy of Rocket Motors Technology - ARMT
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Operator Second Artillery Corps
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# Basing Chuxiong # Jianshui # Lianxiwang # Tonghua
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Configuration Two Stage
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Length [meters] 10.7
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Diameter [meters] 1.4
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Mass [kilograms] 14,700
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Propellant Solid
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Guidance Inertial
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First Flight May 1985
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IOC 1989-1991
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Deployment Mobile
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Range (km) 1,800
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Re-entry Vehicle Mass (kg) 600
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Warhead Yield 200-300 KT
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CEP (meters) 300-400
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Launch Preparation Time 10-15 minutes
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http://www8.janes.com/JDIC/JDET/documentView.do?docId=/content1/janesdata/binder/
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jsws/jsws0411.htm@current&pageSelected=allJanes&keyword=css-5%20df-21&backPath=
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http://jdet.janes.com/JDIC/JDET/search&Prod_Name=JSWS&activeNav=http://www8.janes.com/JDIC/JDET
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DF-21
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Length: 10.7 m
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Body diameter: 1.4 m
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Launch weight: 14,700 kg
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Payload: Single warhead; 600 kg
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Warhead: 250 or 500 kT nuclear, HE, submunitions or chemical
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Guidance: Inertial
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Propulsion: 2-stage solid propellant
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Range: 2,150 km
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Accuracy: 700 m CEP
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DF-21A/-21B
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Length: 12.3 m
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Body diameter: 1.4 m
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Launch weight: 15,200 kg
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Payload: Single warhead, 500 kg
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Warhead: 90 kT or selectable between 20, 90 and 150 kT nuclear, HE,
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chemical, submunitions or EMP
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Guidance: Inertial with GPS and radar correlation
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Propulsion: 2-stage solid propellant
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Range: 2,500 km
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Accuracy: 50 m CEP (21A), 10 m CEP (21B)
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http://www.astronautix.com/lvs/df21.htm
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Intermediate range ballistic missile.
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IOC: 1988.
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Country: China.
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Status: Active.
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Department of Defence Designation: CSS-5.
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Popular Name: Dong Feng-21.
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JL-1 land based version. 2 stage vehicle.
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Manufacturer: Shanxi.
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Launches: 15. Failures: 3.
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Success Rate: 80.00%.
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First Launch Date: 1985-05-01.
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Last Launch Date: 2007-01-11.
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Launch data is: continuing.
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Apogee: 500 km (310 mi).
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Liftoff Thrust: 0 N ( lbf).
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Total Mass: 14,664 kg (32,328 lb).
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Core Diameter: 1.40 m (4.50 ft).
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Total Length: 10.43 m (34.21 ft).
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Span: 1.40 m (4.50 ft).
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Standard warhead mass: 600 kg (1,320 lb).
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Maximum range: 1,810 km (1,120 mi).
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Number Standard Warheads: 1.
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Standard warhead yield: 250 KT.
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Boost Propulsion: Solid rocket.
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Guidance: Inertial.
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Total Number Built: 50.
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* Stage1: 1 x JL-1-1.
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Gross Mass: 10,000 kg (22,000 lb).
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Motor: 1 x DF-21-1.
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Length: 6.00 m (19.60 ft).
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Diameter: 1.41 m (4.62 ft).
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Propellants: Solid.
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* Stage2: 1 x DF-21-2.
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Gross Mass: 4,000 kg (8,800 lb).
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Motor: 1 x DF-21-2.
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Length: 4.00 m (13.10 ft).
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Diameter: 1.41 m (4.62 ft).
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END COMMENT
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*/
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# Weapon Definition starts here.
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# script_debug_writes on
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script_debug_writes on
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# Signature data is unknown...
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infrared_signature RED_MRBM_3_INFRARED_SIGNATURE
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constant 1 watts/steradian
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end_infrared_signature
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optical_signature RED_MRBM_3_OPTICAL_SIGNATURE
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constant 1 m^2
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end_optical_signature
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radar_signature RED_MRBM_3_RADAR_SIGNATURE
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constant 1 m^2
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end_radar_signature
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# Weapon effects
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weapon_effects RED_MRBM_3_LETHALITY WSF_GRADUATED_LETHALITY
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radius_and_pk 150 m 1.0
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end_weapon_effects
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########### Aero definitions ##################################################
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aero RED_MRBM_3_STAGE_EMPTY_AERO WSF_AERO # The stage gets a lot of drag...
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reference_area 1.56 m^2 # 1.41 m diameter
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aspect_ratio 4.0
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cl_max 1.5
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# Values estimated from Hoerner's Drag book
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cd_zero_subsonic 0.40
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cd_zero_supersonic 0.45
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mach_begin_cd_rise 0.9
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mach_end_cd_rise 1.30
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mach_max_supersonic 5.00
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end_aero
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aero RED_MRBM_3_STAGE_1_AERO WSF_AERO
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reference_area 1.56 m^2 # 1.41 m diameter
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aspect_ratio 2.0
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cl_max 4.5
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# Values estimated from Hoerner's Drag book
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cd_zero_subsonic 0.10
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cd_zero_supersonic 0.35
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mach_begin_cd_rise 0.95
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mach_end_cd_rise 1.30
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mach_max_supersonic 10.00
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end_aero
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aero RED_MRBM_3_STAGE_2_AERO WSF_AERO
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reference_area 1.56 m^2 # 1.41 m diameter
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aspect_ratio 2.0
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cl_max 4.5
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# Values estimated from Hoerner's Drag book
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cd_zero_subsonic 0.10
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cd_zero_supersonic 0.35
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mach_begin_cd_rise 0.95
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mach_end_cd_rise 1.30
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mach_max_supersonic 10.00
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end_aero
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aero RED_MRBM_3_STAGE_3_AERO WSF_AERO #smaller cone warhead
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reference_area .572 m^2
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aspect_ratio 2.0
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cl_max 4.5
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# Values estimated from Hoerner's Drag book
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cd_zero_subsonic 0.10
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cd_zero_supersonic 0.35
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mach_begin_cd_rise 0.95
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mach_end_cd_rise 1.30
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mach_max_supersonic 10.00
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end_aero
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########### RED_MRBM_3 Mover definition ##########################################
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mover RED_MRBM_3_MOVER WSF_GUIDED_MOVER
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show_status
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update_interval 0.05 secs
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stage 1
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aero RED_MRBM_3_STAGE_1_AERO
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total_mass 10000 kg
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fuel_mass 8000 kg
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specific_impulse 240 sec # The platform script will vary this.
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thrust_duration 52 sec
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end_stage
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stage 2
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aero RED_MRBM_3_STAGE_2_AERO
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pre_ignition_coast_time 3 sec
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total_mass 4000 kg
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fuel_mass 3350 kg
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specific_impulse 240 sec # adjusted for max range of 2000 km
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thrust_duration 46 sec
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pre_separation_coast_time 10 sec
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end_stage
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stage 3 # warhead
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aero RED_MRBM_3_STAGE_3_AERO
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total_mass 400 kg
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fuel_mass 0 kg
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end_stage
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end_mover
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############ RED_MRBM_3 Guidance ##################################################
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############ The values are SPECIFIC to the aero and body mass information####
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processor RED_MRBM_3_GUIDANCE WSF_GUIDANCE_COMPUTER
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#show_status
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#show_evaluations
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phase LAUNCH
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next_phase 200-1000 if target_ground_range < 1000 km
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next_phase 1000-1100 if target_ground_range < 1100 km
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next_phase 1100-1200 if target_ground_range < 1200 km
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next_phase 1200-1300 if target_ground_range < 1300 km
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next_phase 1300-1350 if target_ground_range < 1350 km
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next_phase 1350-1400 if target_ground_range < 1400 km
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next_phase 1400-1450 if target_ground_range < 1450 km
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next_phase 1450-1500 if target_ground_range < 1500 km
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next_phase 1500-1550 if target_ground_range < 1550 km
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next_phase 1550-1600 if target_ground_range < 1600 km
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next_phase 1600-1650 if target_ground_range < 1650 km
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next_phase 1650-1700 if target_ground_range < 1700 km
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next_phase 1700-1750 if target_ground_range < 1750 km
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next_phase 1750-1800 if target_ground_range < 1790 km
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next_phase 1780-1820 if target_ground_range < 1820 km
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next_phase 1810-1840 if target_ground_range < 1840 km
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next_phase 1840-1860 if target_ground_range < 1860 km
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next_phase 1860-1900 if target_ground_range < 1900 km
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next_phase 1900-1950 if target_ground_range < 1950 km
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next_phase 1940-1980 if target_ground_range < 1980 km
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next_phase 1980-2000 if target_ground_range < 2000 km
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next_phase 2000-2050 if target_ground_range < 2100 km
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end_phase
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phase 200-1000
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g_bias 1.1 # 200-1000
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maximum_commanded_g 4 g # 200-1000
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1000-1100
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g_bias 1.2 # 1000
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maximum_commanded_g 5 g # 1000
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1100-1200
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g_bias 1.4 #
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maximum_commanded_g 1 g #
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guidance_delay 8 sec
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1200-1300
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g_bias 1.5 #
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maximum_commanded_g 1 g #
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guidance_delay 9.5 sec
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1300-1350
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g_bias 1.6 #
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maximum_commanded_g 1 g #
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guidance_delay 10 sec
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1350-1400
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g_bias 1.8 # 1200-1400
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maximum_commanded_g 1 g # 1200-1400
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guidance_delay 11 secs # 1200-1400
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1400-1450
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g_bias 3 # 1500
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maximum_commanded_g 1 g # 1500
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guidance_delay 14 secs # 1500
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1450-1500
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g_bias 3.5 # 1500
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maximum_commanded_g 1 g # 1500
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guidance_delay 15.3 secs # 1500
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1500-1550
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g_bias 4.5 # 1500
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maximum_commanded_g 1 g # 1500
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guidance_delay 16.7 secs # 1500
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1550-1600
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g_bias 5 # 1500
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maximum_commanded_g 1 g # 1500
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guidance_delay 17.1 secs # 1500
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1600-1650
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g_bias 5.6 # 1500
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maximum_commanded_g 1 g # 1500
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guidance_delay 17.5 secs # 1500
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1650-1700
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g_bias 6 # 1600-1700
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maximum_commanded_g 1 g # 1600-1700
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guidance_delay 17.7 secs # 1600-1700
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1700-1750
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g_bias 6 # 1700-1750
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maximum_commanded_g 1 g # 1700-1750
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guidance_delay 18 secs # 1700-1750
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1750-1800
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g_bias 7 # 1750-1800
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maximum_commanded_g 1 g # 1750-1800
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guidance_delay 18.4 secs # 1750-1800
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next_phase TERMINAL when phase_time > 101 secs # burnout time
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end_phase
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phase 1780-1820
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g_bias 7 # 1780-1820
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maximum_commanded_g 1 g # 1780-1820
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guidance_delay 18.5 secs # 1780-1820
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next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
phase 1810-1840
|
||
|
|
g_bias 7 # 1810-1840
|
||
|
|
maximum_commanded_g 1 g # 1810-1840
|
||
|
|
guidance_delay 18.7 secs # 1810-1840
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
|
||
|
|
phase 1840-1860
|
||
|
|
g_bias 8 # 1840-1860
|
||
|
|
maximum_commanded_g 1 g # 1840-1860
|
||
|
|
guidance_delay 18.7 secs # 1840-1860
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
|
||
|
|
phase 1860-1900
|
||
|
|
g_bias 8.5 # 1840-1860
|
||
|
|
maximum_commanded_g 1 g # 1840-1860
|
||
|
|
guidance_delay 18.8 secs # 1840-1860
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
phase 1900-1950
|
||
|
|
g_bias 9 # 1860-1950
|
||
|
|
maximum_commanded_g 1 g #
|
||
|
|
guidance_delay 19 secs #
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
phase 1940-1980
|
||
|
|
g_bias 9.2 # 1940-1980
|
||
|
|
maximum_commanded_g 1 g #
|
||
|
|
guidance_delay 19.2 secs #
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
phase 1980-2000
|
||
|
|
g_bias 9.5 # 1980-2000
|
||
|
|
maximum_commanded_g 1 g #
|
||
|
|
guidance_delay 19.4 secs #
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
|
||
|
|
phase 2000-2050
|
||
|
|
g_bias 9.8 #
|
||
|
|
maximum_commanded_g 1 g #
|
||
|
|
guidance_delay 19.6 secs #
|
||
|
|
next_phase TERMINAL when phase_time > 101 secs # burnout time
|
||
|
|
end_phase
|
||
|
|
|
||
|
|
|
||
|
|
phase TERMINAL
|
||
|
|
maximum_commanded_g 2 g
|
||
|
|
end_phase
|
||
|
|
end_processor
|
||
|
|
|
||
|
|
#############STAGE 1 & 2 SPENT STAGES PLATFORM TYPES#########################################
|
||
|
|
platform_type RED_MRBM_3_STAGE1 WSF_PLATFORM
|
||
|
|
icon sam-a_missile
|
||
|
|
mover WSF_NEW_UNGUIDED_MOVER
|
||
|
|
update_interval 0.5 sec
|
||
|
|
show_status
|
||
|
|
aero RED_MRBM_3_STAGE_EMPTY_AERO
|
||
|
|
total_mass 2500 kg
|
||
|
|
end_mover
|
||
|
|
processor fuse WSF_GROUND_TARGET_FUSE
|
||
|
|
end_processor
|
||
|
|
end_platform_type
|
||
|
|
|
||
|
|
weapon RED_MRBM_3_STAGE1 WSF_EXPLICIT_WEAPON
|
||
|
|
launched_platform_type RED_MRBM_3_STAGE1
|
||
|
|
firing_delay 0 secs
|
||
|
|
quantity 1
|
||
|
|
end_weapon
|
||
|
|
|
||
|
|
platform_type RED_MRBM_3_STAGE2 WSF_PLATFORM
|
||
|
|
icon sam-a_missile
|
||
|
|
mover WSF_NEW_UNGUIDED_MOVER
|
||
|
|
update_interval 0.5 sec
|
||
|
|
show_status
|
||
|
|
aero RED_MRBM_3_STAGE_EMPTY_AERO
|
||
|
|
total_mass 30 kg # extremely low to show ballistic fall
|
||
|
|
end_mover
|
||
|
|
processor fuse WSF_GROUND_TARGET_FUSE
|
||
|
|
end_processor
|
||
|
|
end_platform_type
|
||
|
|
|
||
|
|
weapon RED_MRBM_3_STAGE2 WSF_EXPLICIT_WEAPON
|
||
|
|
launched_platform_type RED_MRBM_3_STAGE2
|
||
|
|
quantity 1
|
||
|
|
end_weapon
|
||
|
|
|
||
|
|
|
||
|
|
############### RED_MRBM_3 platform #############################################
|
||
|
|
platform_type RED_MRBM_3 WSF_PLATFORM
|
||
|
|
icon Scud_Missile
|
||
|
|
infrared_signature RED_MRBM_3_INFRARED_SIGNATURE
|
||
|
|
optical_signature RED_MRBM_3_OPTICAL_SIGNATURE
|
||
|
|
radar_signature RED_MRBM_3_RADAR_SIGNATURE
|
||
|
|
weapon_effects RED_MRBM_3_LETHALITY
|
||
|
|
|
||
|
|
mover RED_MRBM_3_MOVER
|
||
|
|
end_mover
|
||
|
|
|
||
|
|
# used to instantiate the stage falling off
|
||
|
|
weapon red_mrbm_3_stage1 RED_MRBM_3_STAGE1
|
||
|
|
quantity 1
|
||
|
|
launch_delta_v -1 0 0 fps
|
||
|
|
end_weapon
|
||
|
|
# used to instantiate the stage falling off
|
||
|
|
weapon red_mrbm_3_stage2 RED_MRBM_3_STAGE2
|
||
|
|
quantity 1
|
||
|
|
launch_delta_v -100 0 00 fps
|
||
|
|
end_weapon
|
||
|
|
|
||
|
|
script void on_stage_separation(int aStage)
|
||
|
|
writeln_d("T=", TIME_NOW, " ", PLATFORM.Name(), ": Stage ", aStage, " separation");
|
||
|
|
if (aStage == 1)
|
||
|
|
{
|
||
|
|
WsfWeapon weapon = PLATFORM.Weapon("red_mrbm_3_stage1");
|
||
|
|
weapon.Fire();
|
||
|
|
}
|
||
|
|
if (aStage == 2)
|
||
|
|
{
|
||
|
|
WsfWeapon weapon = PLATFORM.Weapon("red_mrbm_3_stage2");
|
||
|
|
weapon.Fire();
|
||
|
|
}
|
||
|
|
end_script
|
||
|
|
|
||
|
|
processor guidance RED_MRBM_3_GUIDANCE
|
||
|
|
# show_status
|
||
|
|
guide_to_truth true #TODO TESTING
|
||
|
|
end_processor
|
||
|
|
|
||
|
|
processor fuse WSF_GROUND_TARGET_FUSE
|
||
|
|
end_processor
|
||
|
|
|
||
|
|
processor seeker WSF_PERFECT_TRACKER
|
||
|
|
update_interval 0.5 sec
|
||
|
|
end_processor
|
||
|
|
|
||
|
|
end_platform_type
|
||
|
|
#####################RED_MRBM_3 EXPLICIT WEAPON###################################
|
||
|
|
weapon RED_MRBM_3 WSF_EXPLICIT_WEAPON
|
||
|
|
launched_platform_type RED_MRBM_3
|
||
|
|
tilt 89.9 degrees
|
||
|
|
slew_mode azimuth
|
||
|
|
azimuth_slew_limits -180 deg 180 deg
|
||
|
|
firing_delay 1.0 secs
|
||
|
|
quantity 1
|
||
|
|
end_weapon
|