coyote fact

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FACT SHEET Customer Program Executive Office for Unmanned Aviation and Strike Weapons, PEO(U&W); Aerial Target & Decoy Systems Program Office, (PMA-208) Objectives • Provide a Cost-Effective Target to Simulate both Supersonic Sea Skimming and other emerging Supersonic Anti-Ship Cruise Missile (ASCM) Threats • Support RDT&E of Ship Defense Systems and Support Fleet Training Exercises Operational October 2005 Prime Contractor Orbital Sciences Corporation – Launch Systems Group, Chandler, Arizona Major Subcontractor Aerojet, Camden, AR • Solid Fuel Ducted Rocket Subsystem QUICK FACTS: Coyote in flight GQM-163A Coyote Supersonic Sea Skimming Target Overview On 29 June 2000, Orbital Sciences Corporation, Launch Systems Group was awarded a $34 million Engineering and Manufacturing Development (EMD) contract for the GQM-163A Supersonic Sea Skimming Target (SSST) system. Orbital’s proven Theater Missile Defense (TMD) and National Missile Defense (NMD) ballistic missile target design philosophy of maximizing residual missile assets and off-the-shelf hardware and technology is being applied to cruise missile targets. This approach provides the U.S. Navy with the best value, lowest risk and highest performance GQM-163A system. The GQM-163A MK 70 Booster/Ducted Rocket Sustainer configuration makes judicious use of residual Standard Missile assets and the $80 million U.S. Government investment in solid- fueled ducted rocket/ramjets. The GQM-163A Ducted Rocket Sustainer is based on technology developed by major subcontractor Aerojet (formerly ARC) under the U.S. Air Force’s Variable Flow Ducted Rocket (VFDR) program. The GQM-163A avionics design is based on the Orbital Launch Systems Group’s multi-program Modular Avionics Control Hardware (MACH) System. The MACH flight computer boasts a modern Power PC core hosting a real-time operating system and a flight proven software architecture based on the Company's common object oriented C++ application framework. Following the EMD phase of the GQM-163A program Orbital received follow-on Full Rate Production (FRP) contracts in excess of 80 production targets, with newer targets being produced with the Orbital designed Front End Subsystem (FES), which introduced several robust technology updates to address obsolescence of the older targets. Under the GQM-163A contract, Orbital has an operational launch success rate of 100%, which includes a successful demonstration of a High Diver trajectory, the Orbital designed FES, and the Orbital designed Target Support Test Set (TSTS). For user flexibility, the GQM-163A target is now operationally capable of launching from three different launch sites around the world. GQM-163A Coyote Supersonic Sea Skimming Target

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Page 1: Coyote Fact

FACT SHEET

CustomerProgram Executive Office for Unmanned Aviation and Strike Weapons, PEO(U&W); Aerial Target & Decoy Systems Program Office, (PMA-208)

Objectives•ProvideaCost-EffectiveTarget

to Simulate both Supersonic Sea Skimming and other emerging SupersonicAnti-ShipCruiseMissile(ASCM)Threats

•SupportRDT&EofShipDefenseSystems and Support Fleet Training Exercises

OperationalOctober 2005

Prime ContractorOrbitalSciencesCorporation–LaunchSystemsGroup,Chandler,Arizona

Major Subcontractor

Aerojet, Camden, AR•SolidFuelDuctedRocketSubsystem

QUICK FACTS:

Coyoteinflight

GQM-163A CoyoteSupersonic Sea Skimming Target

OverviewOn29June2000,OrbitalSciencesCorporation,LaunchSystemsGroupwasawardeda$34millionEngineeringandManufacturingDevelopment(EMD)contractfortheGQM-163ASupersonic Sea Skimming Target (SSST) system. Orbital’s proven Theater Missile Defense (TMD) and National Missile Defense (NMD) ballistic missile target design philosophy of maximizingresidualmissileassetsandoff-the-shelfhardwareandtechnologyisbeingappliedtocruisemissiletargets.ThisapproachprovidestheU.S.Navywiththebestvalue,lowestriskandhighestperformanceGQM-163Asystem.

TheGQM-163AMK70Booster/DuctedRocketSustainerconfigurationmakesjudicioususeofresidualStandardMissileassetsandthe$80millionU.S.Governmentinvestmentinsolid-fueledductedrocket/ramjets.TheGQM-163ADuctedRocketSustainerisbasedontechnologydevelopedbymajorsubcontractorAerojet(formerlyARC)undertheU.S.AirForce’sVariableFlowDuctedRocket(VFDR)program.TheGQM-163AavionicsdesignisbasedontheOrbitalLaunchSystemsGroup’smulti-programModularAvionicsControlHardware(MACH)System.TheMACHflightcomputerboastsamodernPowerPCcorehostingareal-timeoperatingsystemandaflightprovensoftwarearchitecturebasedontheCompany'scommonobjectorientedC++applicationframework.

FollowingtheEMDphaseoftheGQM-163AprogramOrbitalreceivedfollow-onFullRateProduction(FRP)contractsinexcessof80productiontargets,withnewertargetsbeingproducedwiththeOrbitaldesignedFrontEndSubsystem(FES),whichintroducedseveralrobusttechnologyupdatestoaddressobsolescenceoftheoldertargets.UndertheGQM-163Acontract,Orbitalhasanoperationallaunchsuccessrateof100%,whichincludesasuccessfuldemonstrationofaHighDivertrajectory,theOrbitaldesignedFES,andtheOrbitaldesignedTargetSupportTestSet(TSTS).Foruserflexibility,theGQM-163Atargetisnowoperationallycapableoflaunchingfromthreedifferentlaunchsitesaroundtheworld.

GQM-163ACoyoteSupersonicSeaSkimmingTarget

Page 2: Coyote Fact

Orbital Sciences Corporation | 3380 South Price Road | Chandler, Arizona 85248 | www.orbital.com

©2011OrbitalSciencesCorporation.BR06007c

GQM-163A Coyote

Representative GQM-163A Mission Profile and System Performance

For more information, please contact:

Mark OgrenVPofBusinessDevelopment 480.814.6605 [email protected]

Booster Air Vehicle

0.0

87.2

in.

(2.2

1 m

)

154.

6 in

.(3

.93

m)

221.

2 in

.(5

.62

m)

232.

3 in

.(5

.90

m)

376.

2 in

.(9

.56

m )

Aft Launch Lug

17.99 in. DIA(0.46 m) 13.8 in. DIA

(0.35 m)

Booster IgniterMK301 Mod 1

Fin ActuatorController System (4)

Fairing Assembly

Forward Launch Lugs

Solid Hydro-carbon Fuel Gas Generator

Booster Fin Set BoosterMK 70 Mod 1

Four Air Inlets

FourRaceways

Nosecone

Combustion Chamber

Guidance & MissionEquipment Section

MK 70 DR FES

Ballast

Manacle Clamp

Ducted Rocket Burnout Alt = 13 ft

Begin Cruise Alt = 65 ft

Apogee Alt = 1800 ftBooster

SeparationAlt = 1200 ft

Alt = 15 ft

Ignite MK 70 BoosterLauncher 35 nmi

Cruise Phase Mach 2.5

30° Dive

20 nmi - 120 nmi Mach 3.0 - 4.0

Begin Cruise Alt = 35,000 ft - 60,000 ft

Begin Dive

10 nmi Terminal Phase

Mach 2.5