Editing Delta-glider
Jump to navigation
Jump to search
Warning: You are not logged in. Your IP address will be publicly visible if you make any edits. If you log in or create an account, your edits will be attributed to your username, along with other benefits.
The edit can be undone. Please check the comparison below to verify that this is what you want to do, and then save the changes below to finish undoing the edit.
| Latest revision | Your text | ||
| Line 15: | Line 15: | ||
|wing_area=160 m<sup>2</sup> | |wing_area=160 m<sup>2</sup> | ||
|empty_mass=12,000 kg | |empty_mass=12,000 kg | ||
| − | |fuel_mass= | + | |fuel_mass=11,400 kg |
|rcs_fuel_mass=600 kg | |rcs_fuel_mass=600 kg | ||
| − | |max_takeoff_mass= | + | |max_takeoff_mass=24,000 kg |
|inertia_pmi=15.5 / 22.1 / 7.7 m<sup>2</sup> | |inertia_pmi=15.5 / 22.1 / 7.7 m<sup>2</sup> | ||
|main_engine_template=Engine | |main_engine_template=Engine | ||
| Line 31: | Line 31: | ||
|rcs_engine=16 x 1 kN | |rcs_engine=16 x 1 kN | ||
|rcs_engine_isp=40 kN·s/kg | |rcs_engine_isp=40 kN·s/kg | ||
| − | |max_deltav= | + | |max_deltav=59.9 km/s |
|max_accel=20 m/s<sup>2</sup> | |max_accel=20 m/s<sup>2</sup> | ||
|airfoil_performance_template=AirfoilPerformance | |airfoil_performance_template=AirfoilPerformance | ||
| Line 46: | Line 46: | ||
and landings independent of atmospheric conditions and runways. | and landings independent of atmospheric conditions and runways. | ||
| − | + | It comes with the stock Orbiter install. | |
| − | + | There´s also a Scramjet version, the [[Delta-glider-S]]. | |
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||