Analysis of information sources in references of the Wikipedia article "軌道發射系統比較" in Chinese language version.
|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
Currently, two versions of PSLV are operational, namely PSLV-XL (with six extended version of Strap-on motors) and the PSLV Core-alone (without Strap-on motors).
Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)Ariane 5 set a new record in June 2017 by lofting 10,865 kg. into geostationary transfer orbit (GTO). From this payload lift record, Ariane 5's performance will be increased another 250 kg.
Russian officials have said they plan to discontinue Dnepr launches.
LEO Payload 200 x 1,600 km x 143 deg – Shavit: 160 kg – Shavit-1: 225 kg – Shavit-2: 300 kg
|url-status=和|dead-url=只需其一 (帮助)Ariane 5 set a new record in June 2017 by lofting 10,865 kg. into geostationary transfer orbit (GTO). From this payload lift record, Ariane 5's performance will be increased another 250 kg.
Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
Orbex can accommodate a range of payload capacities between 100kg-220kg, to altitudes of between 200km-1250km.
LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
LEO Payload 200 x 1,600 km x 143 deg – Shavit: 160 kg – Shavit-1: 225 kg – Shavit-2: 300 kg
|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)Russian officials have said they plan to discontinue Dnepr launches.
|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)|url-status=和|dead-url=只需其一 (帮助)Currently, two versions of PSLV are operational, namely PSLV-XL (with six extended version of Strap-on motors) and the PSLV Core-alone (without Strap-on motors).
BFR in fully reusable configuration, without any orbital refueling, we expect to have a payload capability of 150 tonnes to low Earth orbit and that compares to about 30 for Falcon Heavy