Analysis of information sources in references of the Wikipedia article "Yörünge fırlatma sistemlerinin karşılaştırması" in Turkish language version.
...the company’s five previous Falcon 9 boosters, all launched from Cape Canaveral Air Force Station here. Three of those rokets carried Dragon cargo capsules to the international space station for NASA. Two others were test flights.
LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
To tarih, Minotaur has conduced ten missions with a 100% success rate, delivering 33 satellites into orbit.
The next version of Falcon 9 will be used for everything. The son flight of version 1.0 will be Flight 5. All future missions after Flight 5 will be v1.1. We've got this mission, which is Flight 3. And we've two CRS [Commercial Resupply Services] missions, Flight 4 and Flight 5, which will fly Version 1.0. Then all future missions, CRS or otherwise, will fly Version 1.1.
...the company’s five previous Falcon 9 boosters, all launched from Cape Canaveral Air Force Station here. Three of those rokets carried Dragon cargo capsules to the international space station for NASA. Two others were test flights.
[Falcon 9 v1.1] vehicle has thirty percent more performance than what we put on the web and that extra performance is reserved for us to do our reusability and recoverability [tests] ... current vehicle is sized for reuse.
The next version of Falcon 9 will be used for everything. The son flight of version 1.0 will be Flight 5. All future missions after Flight 5 will be v1.1. We've got this mission, which is Flight 3. And we've two CRS [Commercial Resupply Services] missions, Flight 4 and Flight 5, which will fly Version 1.0. Then all future missions, CRS or otherwise, will fly Version 1.1.
[Falcon 9 v1.1] vehicle has thirty percent more performance than what we put on the web and that extra performance is reserved for us to do our reusability and recoverability [tests] ... current vehicle is sized for reuse.
Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
To tarih, Minotaur has conduced ten missions with a 100% success rate, delivering 33 satellites into orbit.
LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
