I designed a super sonic Otomat for you.
RAM-Otomat SUPER (EXCLUDING BOOSTER)
Control system: v5 TTWCS - Next Generation Tactical Tomahawk Weapon Control System (2006)
-OR-
TESEO/ERATCO Otomat Control Systems w/ PRT-400 data-uplink support
Guidance:
Active Radar-AESA w/ Low Probability of Intercept
&
IR+Inertial Guidance
Unit price: $1.76 million USD
Length: 18.01 ft
Diameter: 1.6 ft
Wing-span: 12 ft
Wing area: 59 ft
Wing-loading: 49 lbs/sq ft
Wing Sweep: 67 degrees (once wings unfold)
*Has 4 tail fins (guidance) and 2 canards (attack angle control)*
Launch weight: 2,900 lbs
Operating weight: 2,600 to 2,900 lbs
Light weight: 2,598 lbs
Warhead: 450 lbs (204 kg)
Max fuel: 302 lbs
Powerplant: Super Zumo Z-1
variable-cycle geared-turbofan
Intake-Diameter: 0.9 ft
Bypass ratio: 0.8
Variable-geomeetry intake: 0.3 ft
Specific Fuel Consumption (SFC): 1.35 lbs/lb thrust/hr
Exhaust Velocity: 1,031 m/s (absolute)
Intake velocity: 243 m/s (relative to aircraft)
Thrust: 4,085 lbs (16,278 hp)
Typical weight: 917 lbs
PERFORMANCE:
Stall speed at 2,900 lbs: 138 kts TAS (138 kts IAS)
@ 2,900 lbs (in flight)
Maximum Flight Ceiling: 70,800 ft @ 1,500 kts (Mach 2.6, 1,725 mph)
@ 55,000 ft ASL
Maximum Speed: 2,100 kts TAS (739 kts IAS) (Mach 3.64)
@ 50,000 ft ASL
Maximum Speed: 2,080 kts TAS (823 kts IAS) (Mach 3.61)
(throttle 99%)
@ 1,000 ft ASL
Maximum Speed: 1,315 kts TAS (1,300 kts IAS) (Mach 1.99)
(throttle 99%)
@ 65 ft ASL
Maximum Speed: 1,305 kts (1,304 kts IAS) (Mach 1.97)
(throttle 99%)
Range Tables:
@70,000 ft ASL
& 1,000 kts = 586 nmi
& 1,200 kts = 618 nmi
@ 60,000 ft ASL
& 1,000 kts = 565 nmi
& 1,200 kts = 444 nmi
& 1,500 kts = 389 nmi (Mach 2.6)
& 1,700 kts = 351 nmi (Mach 2.95) (throttle 89%)
& 1,900 kts = 312 nmi (Mach 3.12) (throttle 100%)
@ 50,000 ft ASL
& 890 kts = 490 nmi (throttle 39%) (Mach 1.54 supercruise)
& 1,000 kts = 468 nmi (throttle 40%) (Mach 1.74 supercruise)
& 1,200 kts = 351 nmi (throttle 54%)
& 1,300 kts = 328 nmi
& 1,500 kts = 287 nmi
& 1,700 kts = 248 nmi
& 2,000 kts = 199 nmi
& 2,050 kts = 193 nmi (99% throttle)
@ 1,000 ft ASL
& 1,000 kts = 113 nmi
& 1,050 kts = 106 nmi
& 1,125 kts = 96 nmi
& 1,200 kts = 88 nmi
& 1,300 kts = 76 nmi
@ 65 ft ASL
200 kts = 139 nmi
400 kts = 255 nmi
555 kts = 215 nmi
1,000 kts = 111 nmi
1,200 kts = 86 nmi
1,300 kts = 74 nmi
@ 2,615 lbs (in-flight-END of trajectory) (2,598 lbs is the light weight/no fuel weight)
@ 65 ft ASL
Maximum Speed: 1,636 kts (1,635 kts IAS) (Mach 2.47)
(throttle 100%)
comparison of specific fuel consumption @ an altitude of 65 ft above sea level.
139 kts: 1.45 lbs/lb thrust/hr
200 kts: 1.50 lbs/lb thrust/hr
400 kts: 1.65 lbs/lb thrust/hr
800 kts: 2.00 lbs/lb thrust/hr (412 m/s)
1000 kts: 2.19 lbs/lb thrust/hr (515 m/s)
1300 kts: 2.49 lbs/lb thrust/hr (670 m/s)
Variable-geometry intake:
@ 65 ft ASL
& 200 kts = 0.604 ft
& 400 kts = 0.604 ft
& 1,000 kts = 0.604 ft
& 1,200 kts = 0.565 ft
& 1,400 kts = 0.523 ft
& 1,500 kts = 0.505 ft
& 1,636 kts = 0.484 ft
@ 50,000 ft ASL
*intake same from 400 kts to 3000 kts*
& 800 kts = 0.860 ft
@ 1,000 kts = 0.860 ft
@ 3,000 kts = 0.860 ft
*Aircraft is incapable of travelling at 3,000 kts, statistic merely to illustrate geo-
variable intake efficiency*
@ 70,000 ft ASL
& 1,500 kts = 0.840 ft
*Intake diameter does not change at this altitude anywhere below 7,000 kts!*
Production & Unit Price per order:
100 units: $1.859 million USD
500 units: $1.762 million USD
800 units: $1.659 million USD
_________________ "All your base are belong to us"
Last edited by CATZ on May 21st, 2011, 7:13 pm, edited 1 time in total.
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