Orbital GQM-163A Coyote - Manual (Page 2)

GQM-163A Coyote
Representative GQM-163A Mission Profile and System Performance
More Information
Mark Ogren
VP of Business Development
(480) 814-6605
[email protected]
Booster Air Vehicle
0.0
87.2 in (2.21 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 Igniter
MK301 Mod 1
Fin Actuator
Controller System (4)
Fairing Assembly
Forward Launch Lugs
Solid Hydro-carbon Fuel Gas
Generator
Booster Fin Set
Booster
MK 70 Mod 1
Four Air Inlets
Four
Raceways
Nosecone
Combustion
Chamber
Guidance & Mission
Equipment Section
MK 70 DR FES
Ballast
Manacle Clamp
Ducted Rocket Burnout
Alt = 13 ft
Begin Cruise
Alt = 65 ft
Apogee
Alt = 1800 ft
Booster
Separation
Alt = 1200 ft
Alt = 15 ft
Ignite MK 70 Booster
Launcher
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
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