Kuaizhou-1A-Pro (KZ-1A-Pro)

Kuaizhou-1A-Pro (Airsat 08) [EXPACE]

The Kuaizhou-1 launcher, developed by China Aerospace Science and Technology Corporation (CASIC), is a small, solid fueled launch vehicle, which is possibly based on the road mobile DF-21 IRBM with two additional upper stages.

The Kuaizhou-1 vehicle consits of three solid fueled stages and a fourth liquid fueled stage.

The vehicle is reportedly designed for quick-reaction launches and can reportedly place 400 kg into orbit. The payload of Kuaizhou-1 is integrated with the upper stage.

A commercial variant is offered under the designation Fei Tian 1 (FT-1). This one offers a separable payload and a larger payload fairing. Another version, Kuaizhou-1A appears to be similar, also offering separable payloads. Possibly, these names refer both to the same version.

An upgraded version called Kuaizhou-1A-Pro (formerly Kuaizhou-1B) with larger diameter stage (1.4 m), a restartable stage 4, and wider fairing (1.8 m) has been introduced in December 2024. Notably stage 4 is mounted upside-down above the payload.

→ complete list of all Kuaizhou-1 flights

Version Stage 1 Stage 2 Stage 3 Stage 4
Kuaizhou-1A (KZ-1A) ? ? ? ?
Performance (kg) LEO LPEO SSO GTO GEO MolO IP
Kuaizhou-1A-Pro (Kuaizhou-1B) 500 450 360 - - - -
No:   TNr:  Type:             Serial    Date           LS              Payload

31     1    Kuaizhou-1A-Pro   Y32       04.12.2024     Xi MLP          AIRSAT 08 (Haishao 1)
32     2    Kuaizhou-1A-Pro ? Y33       01.03.2025  F  Jq LC-43/95A    ?
33     3    Kuaizhou-1A-Pro   Y.        31.07.2025     Xi MLP          PRSC S1
34     4    Kuaizhou-1A-Pro   Y.        05.12.2025     Jq LC-43/95A    Jiaotong VDES A / Jiaotong VDES B


Planned:

 
Failures:


Launch sites:

Jq  =    Jiuquan Space Center, Inner Mongolia, China   China
TY  =    Taiyuan Satellite Launch Center (TSLC), Wuzhai, Shanxi, China   China
Xi  =    Xichang Space Center (Songlin), Sichuan, China   China

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