[China Aerospace Science and Industry Corp.] [Launch vehicles Technology Research Institute] [Vice-President] [Zhang Di] on 11th in Wuhan said to be in [this December] with [KZ-1 rocket] launch ["Jilin One"] [smart video satellite 03 Star] and [two cubes Star]. [KZ-11 launch vehicle] will be the first commercial launch in 2017.
I'd understand this as Quote[China Aerospace Science and Industry Corp.] [Launch vehicles Technology Research Institute] [Vice-President] [Zhang Di] on 11th in Wuhan said to be in [this December] with [KZ-1 rocket] launch ["Jilin One"] [smart video satellite 03 Star] and [two cubes Star]. [KZ-11 launch vehicle] will be the first commercial launch in 2017.So the main payload would be Lingqiao Shipin 03 of the Jilin-1 family of satellites. Two previous smart video satellites were launched with Jilin-1 per se.
Does that mean that Lingqiao A and Lingqiao B are actually Lingqiao 1-01 and Lingqiao 1-02, respectively?
Does anyone know, what the differences between Kuaizhou-1A and Kuaizhou-1 are? Kuaizhou-1A for seperable payloads and Kuaizhou-1 for payloads integrated with the final stage?
According to Chinaspaceflight.com the launch was delayed to January 2017.
Sats on this launch are Jilin-1 (3), Xingyun Shiyan-1 and Kaidun-1 'Canton-1'.Jilin-1 (3) is a high resolution video observation satellite.Kaidun-1 will be used for maritime management (?)
We could really use some photos, anything, even in processing, of this vehicle. I'm struggling
From the Users Guide, the N2O4/MMH bipropellant fourth stage "Propulsion Control Module" appears to perform an initial separation burn from the third stage, followed by a several minute coast and, finally, a 5 to 6 minute long insertion burn for 700 km SSO missions. At 0.4 g maximum acceleration, I would guess that the propulsion system provides 100 to 200 kgf thrust. The module also appears to provide pitch/yaw/roll control during Stage 2 and 3 phases, including coast.Any information on the solid motor stage thrusts? - Ed Kyle
Quote from: edkyle99 on 01/09/2017 03:11 pmFrom the Users Guide, the N2O4/MMH bipropellant fourth stage "Propulsion Control Module" appears to perform an initial separation burn from the third stage, followed by a several minute coast and, finally, a 5 to 6 minute long insertion burn for 700 km SSO missions. At 0.4 g maximum acceleration, I would guess that the propulsion system provides 100 to 200 kgf thrust. The module also appears to provide pitch/yaw/roll control during Stage 2 and 3 phases, including coast.Any information on the solid motor stage thrusts? - Ed Kyletry page 17 Table 2.1 in the L2 posted KZ1A UG
From what I gather from CCTV the main paylod was Jilin-1 (03). I think that's strange since Jilin-1 (01) was launched on a CZ-2D and there does not seem to be a Jilin-1 (02). Plus Jilin-1 (01) seemd too heavy to be launched on a KZ-1A. Any idea on what Jilin-1 (03) really is? Gunter's space page has is as http://space.skyrocket.de/doc_sdat/lingqiao.htm