Altea erospace XR Flight, Руководство по эксплуатации

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XR Flight Operations Manual Version 3.0
Copyright 2006-2018 Douglas Beachy. All Rights Reserved. 69
Empty Mass 12,000 kg 16,080 kg 266,400 kg
Main Fuel Mass 10,400 kg 13,396 kg 230,880 kg
RCS Fuel Mass 600 kg 804 kg 13,320 kg
SCRAM Fuel Mass 2,500 kg 3,350 kg 55,500 kg
APU Fuel Mass 200 kg 268 kg 4,440 kg
LOX Mass
5
(see footnote) 65 kg (7 days)
to 3389 kg (5
years)
182 kg (7
days) to
47,438 kg (5
years)
234 kg (7 days)
to 60,991 kg (5
years)
Fully Loaded Mass w/14-day LOX and full
crew complement (no cargo) 26,254 kg 35,748 kg 572,225 kg
Length 17.76 meters 23.91 meters 60.34 meters
Wingspan 17.86 meters 18.95 meters 76.67 meters
Rear Gear Track 6.82 meters 7.48 meters 35.61 meters
Payload Bay Capacity N/A 3 custom
payload slots
(approx. 30
cubic meters)
36 Standard
Cargo slots
(approx. 2,500
cubic meters)
Maximum Payload Mass N/A 10,795 kg
(max
recommended)
432,000 kg
(max
recommended)
Main Engine Thrust in Vacuum 192 kN x 2
384 kN total
302 kN x 2
605 kN total
1,420 kN x 6
8,524 kN total
Hover Engine Thrust in Vacuum 88 kN x 3
264 kN total
208 kN x 2
415 kN total
977 kN x 6
5,860 kN total
Maximum SCRAM Engine Thrust ~160 kN x 2
~320 kN total
~350 kN x 2
~700 kN total
~5,250 kN x 2
~10,500 kN
total
Retro Engine Thrust in Vacuum 40.8 kN x 2
81.6 kN total
64.2 kN x 2
129 kN total
905 kN x 2
1,811 kN total
SCRAM Diffuser Thermal Limit 8000° Kelvin 8000° Kelvin 8000° Kelvin
APU Runtime (“low”
APUFuelBurnRate
default setting)
~110 minutes ~110 minutes ~110 minutes
APU Startup/Shutdown time 2.5 seconds
(nominal)
2.5 seconds
(nominal)
2.5 seconds
(nominal)
Principal Moments of Inertia (PMI) 15.5 / 22.1 /
7.77
32.04 / 42.56 /
13.17
317.35 / 305.08
/ 219.45
Cross Sections 55.13 / 190.53 /
26.41
77.46 / 238.98
/ 30.14
543.82 /
1962.75 /
330.97
Center of Mass (in meters) 0.0, -0.07,
-0.50
0.0, 0.41,
-2.05
0.0, 10.45,
-4.66
Crew Complement 5 14 18
Gear deployment time 6.7 seconds 6.7 seconds 6.7 seconds
Docking Port / Nosecone deployment time 20.0 seconds 20.0 seconds 20.0 seconds
Crew Elevator deployment time N/A N/A 35.0 seconds
Airlock doors opening time 10.0 seconds 10.0 seconds 10.0 seconds
5 The maximum LOX listed here assumes that LOXConsumptionRate in the config file
is set to its default of AUTO ; the amount of LOX loaded will be higher if
LOXConsumptionRate is changed. For example, if LOXConsumptionRate is set to
Realistic , the actual LOX loaded for a five-year mission would be 16,942 kg (37,350
pounds).