Difference between revisions of "Salamander"
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| '''Lifting capacity''' | | '''Lifting capacity''' | ||
'''(Earth to Moon):''' | '''(Earth to Moon):''' | ||
− | | | + | | 27 metric tons plus 15 passengers, or 42 metric tons |
|- | |- | ||
| '''Cargo configuration:''' | | '''Cargo configuration:''' | ||
Line 52: | Line 52: | ||
| '''Cargo capacity''' | | '''Cargo capacity''' | ||
'''(LEO to Earth):''' | '''(LEO to Earth):''' | ||
− | | 6 TEU containers, up to | + | | 6 TEU containers, up to 70 tons total cargo mass (max 15% fuel for reentry) |
|- | |- | ||
| '''Length:''' | | '''Length:''' | ||
− | | | + | | 12 days launch to landing |
|- | |- | ||
| '''Emergency life support reserve:''' | | '''Emergency life support reserve:''' | ||
Line 73: | Line 73: | ||
| '''Passenger capacity:''' | | '''Passenger capacity:''' | ||
| Up to 60 passengers in g-couch luxury seating. | | Up to 60 passengers in g-couch luxury seating. | ||
− | Special | + | Special 5-TEU short-term passenger transport unit required (40 tons). |
+ | |- | ||
+ | | '''Required cargo:''' | ||
+ | | 1 extended life support services TEU (28 tons) -- provides necessary life support for passengers, 3,000 kg baggage area, and 15 tons of auxillary fuel | ||
|- | |- | ||
| '''Length:''' | | '''Length:''' | ||
Line 92: | Line 95: | ||
| 2 pilots, 1 flight engineer | | 2 pilots, 1 flight engineer | ||
|- | |- | ||
− | | '''Additional crew if passengers:''' | + | | '''Additional crew if carrying passengers:''' |
| 1 flight surgeon or medical officer, 2 passenger liaisons (flight attendants) | | 1 flight surgeon or medical officer, 2 passenger liaisons (flight attendants) | ||
|- | |- | ||
| '''Passenger capacity:''' | | '''Passenger capacity:''' | ||
− | | Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required. | + | | Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required (15 tons). |
|- | |- | ||
| '''Cargo capacity:''' | | '''Cargo capacity:''' | ||
− | | | + | | 3 TEU/27 tons total (5 TEU/42 tons total if no passenger transport unit) |
|- | |- | ||
| '''Required cargo:''' | | '''Required cargo:''' | ||
− | | 1 | + | | 1 extended life support services TEU (28 tons) |
|- | |- | ||
| '''Length:''' | | '''Length:''' | ||
Line 125: | Line 128: | ||
|- | |- | ||
| '''Passenger capacity:''' | | '''Passenger capacity:''' | ||
− | | Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required. | + | | Up to 15 passengers in coach seating. Special 2-TEU medium-term passenger transport unit required (15 tons). |
|- | |- | ||
| '''Cargo capacity:''' | | '''Cargo capacity:''' | ||
− | | | + | | 3 TEU/27 tons total (5 TEU/42 tons total if no passenger transport unit) |
|- | |- | ||
| '''Required cargo:''' | | '''Required cargo:''' | ||
− | | 1 | + | | 1 extended life support services TEU (28 tons) |
|- | |- | ||
| '''Length:''' | | '''Length:''' | ||
− | | 7 days from | + | | 7 days from Moon launch to LEO |
|- | |- | ||
| '''Emergency life support reserve:''' | | '''Emergency life support reserve:''' | ||
| 3 weeks max for 15 passengers | | 3 weeks max for 15 passengers | ||
|} | |} |
Revision as of 10:48, 30 April 2007
The Salamander
Dry mass: | 120 metric tons |
Fuel capacity: | 60 metric tons |
Wingspan: | 48.75 meters |
Length: | 48.78 m |
Height (gear up): | 6.01 m |
Height (gear down): | 7.57 m |
Lifting capacity
(Earth to LEO): |
70 metric tons or 60 passengers |
Lifting capacity
(Earth to Moon): |
27 metric tons plus 15 passengers, or 42 metric tons |
Cargo configuration: | Up to 6 TEU units in any combination (mass limited by 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 70 tons total cargo mass (max 15% fuel for reentry) |
Length: | 12 days launch to landing |
Emergency life support reserve: | 4-5 weeks |
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 5-TEU short-term passenger transport unit required (40 tons). |
Required cargo: | 1 extended life support services TEU (28 tons) -- provides necessary life support for passengers, 3,000 kg baggage area, and 15 tons of auxillary fuel |
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 |
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 (15 tons). |
Cargo capacity: | 3 TEU/27 tons total (5 TEU/42 tons total if no passenger transport unit) |
Required cargo: | 1 extended life support services TEU (28 tons) |
Length: | 7 days from Earth launch to Moon landing |
Emergency life support reserve: | 3 weeks max for 15 passengers |
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 (15 tons). |
Cargo capacity: | 3 TEU/27 tons total (5 TEU/42 tons total if no passenger transport unit) |
Required cargo: | 1 extended life support services TEU (28 tons) |
Length: | 7 days from Moon launch to LEO |
Emergency life support reserve: | 3 weeks max for 15 passengers |