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− | = | + | =The Salamander= |
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− | + | {| class="wikitable" border="1" cellpadding="2" cellspacing="0" | |
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− | {| class="wikitable" border="1" cellpadding="2" cellspacing="0 | ||
|+ '''Specifications:''' | |+ '''Specifications:''' | ||
+ | |- | ||
+ | | '''Dry mass:''' | ||
+ | | 120 metric tons | ||
+ | |- | ||
+ | | '''Fuel capacity:''' | ||
+ | | 60 metric tons | ||
|- | |- | ||
| '''Wingspan:''' | | '''Wingspan:''' | ||
Line 35: | Line 23: | ||
| 7.57 m | | 7.57 m | ||
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− | | ''' | + | | '''Lifting capacity Earth to LEO:''' |
− | | | + | | 70 metric tons or 60 passengers |
|- | |- | ||
− | | ''' | + | | '''Lifting capacity Earth to Moon:''' |
− | | | + | | 25 metric tons plus 15 passengers, or 40 metric tons |
|- | |- | ||
− | | ''' | + | | '''Cargo configuration:''' |
− | | | + | | Up to 6 TEU units in any combination |
− | | | + | (mass limited by mission profile) |
− | | ''' | + | |} |
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+ | |||
+ | {| class="wikitable" border="1" cellpadding="2" cellspacing="0" | ||
+ | |+ '''Earth cargo mission profile:''' | ||
+ | |- | ||
+ | | Summary: | ||
+ | | Launch from Earth to LEO up to 1200 km circular orbit. Optionally load with additional cargo for return to Earth. | ||
|- | |- | ||
− | | | + | | Crew: |
− | | | + | | 2 pilots and 1 flight engineer |
|- | |- | ||
− | | | + | | Cargo capacity (Earth to LEO): |
− | | | + | | 6 TEU containers, up to 70 tons total cargo mass |
|- | |- | ||
− | | | + | | Cargo capacity (LEO to Earth): |
− | | | + | | 6 TEU containers, up to 30 tons total cargo mass |
|- | |- | ||
− | | | + | | Length: |
− | | | + | | 5-10 days, depending upon launch window |
|- | |- | ||
− | | | + | | Emergency life support reserve: |
− | + | | 4-5 weeks | |
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|} | |} | ||
− | + | '''Earth passenger mission profile:''' | |
− | + | * Summary: Transport passengers from Earth to LEO and back. | |
+ | * Crew: 2 pilots, 1 flight engineer, 1 flight surgeon or medical officer, 2 passenger liaisons (flight attendants) | ||
+ | * Passenger capacity: Up to 60 passengers in g-couch luxury seating. Special 6-TEU short-term passenger transport unit required. | ||
+ | * Length: 12 hours nominal launch-to-rendezvous, 8 days docked (6 months if in safe-mode), 12 hours from undock to touchdown | ||
+ | * Emergency life support reserve: 2 weeks for 60 passengers | ||
+ | |||
+ | |||
+ | '''Earth-to-Moon transport mission profile:''' | ||
+ | * Summary: Transport passengers and cargo from Earth to Moon | ||
+ | * Crew: 2 pilots, 1 flight engineer | ||
+ | * Additional crew if carrying passengers: 1 flight surgeon or medical officer, 2 passenger liaisons (flight attendants) | ||
+ | * Passenger capacity: Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required. | ||
+ | * Cargo capacity: 2 TEU/25 tons total (4 TEU/ if no passenger transport unit) | ||
+ | * Required cargo: 1 fuel TEU, 1 life support services TEU | ||
+ | * Length: 7 days from Earth launch to Moon landing | ||
+ | * Emergency life support reserve: 3 weeks max for 15 passengers | ||
+ | |||
+ | |||
+ | '''Moon-to-LEO transport mission profile:''' | ||
+ | * Summary: Transport passengers and cargo from Moon to Earth | ||
+ | * Crew: 2 pilots, 1 flight engineer | ||
+ | * Additional crew if carrying passengers: 1 flight surgeon or medical officer, 2 passenger liaisons (flight attendants) | ||
+ | * Passenger capacity: Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required. | ||
+ | * Cargo capacity: 2 TEU containers (4 if no passenger transport unit) | ||
+ | * Required cargo: 1 fuel TEU, 1 life support services TEU | ||
+ | * Length: 7 days from Earth launch to Moon landing | ||
+ | * Emergency life support reserve: 3 weeks max for 15 passengers |