Kaituozhe-1B
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The Kaituozhe ( zh, s=开拓者, p=kāi tuò zhě, l=''pioneer'') or ''KT'' rocket family is a series of launch vehicles built by the
China Aerospace Science and Technology Corporation The China Aerospace Science and Technology Corporation, or CASC, is the main contractor for the Chinese space program. It is state-owned and has subsidiaries which design, develop and manufacture a range of spacecraft, launch vehicles, strategi ...
(CASC).


Kaituozhe-1

Kaituozhe-1 (KT-1) was small, solid fueled launch vehicle based on the road mobile
DF-21 The Dong-Feng 21 (DF-21; NATO reporting name CSS-5 - Dong-Feng () is a two-stage, solid-fuel rocket, single-warhead medium-range ballistic missile (MRBM) in the Dong Feng series developed by China Changfeng Mechanics and Electronics Technology A ...
IRBM with an additional upper stage (in total 4 stages). It was 13.6 meters in length and 1.4 meters in diameter, with launch mass of 20t. It was possible to launch KT-1 both from a truck-based platform or from airborne platform. It had a 100 kg to LEO payload capacity. It was possibly the launch vehicle for a Chinese ASAT system that was tested against an old Chinese weather satellite in 2007. The vehicle has performed two flights, the first on 15 September 2002 and the second 16 September 2003. The first flight failed to place a 50 kg
satellite A satellite or artificial satellite is an object intentionally placed into orbit in outer space. Except for passive satellites, most satellites have an electricity generation system for equipment on board, such as solar panels or radioiso ...
into polar orbit due to a second stage malfunction. The second flight was also a failure, however Chinese officials declared some success citing the guidance systems, fairing separation and satellite-launcher separation as successful. The second launch sent the payload, PS-2 microsatellite (40 kg) into wrong orbit. The satellite completed barely one orbit before re-entering the atmosphere. The Kaituozhe-1 launcher appears to have been cancelled after two unsuccessful launches. A third (in 2004) and fourth launch have been rumored, but are not confirmed. The rocket had three variants: the Kaituozhe-1 (KT-1), the Kaituozhe-1A (KT-1A, originally designated KT-2, not to be confused with KT-2 below) and the Kaituozhe-1B (KT-1B, originally designated KT-2A, not to be confused with KT-2A below). The rockets that flew were of the KT-1 variant. The KT-1A and KT-1B variant rockets were not built.


Kaituozhe-2

Like its predecessor the Kaituozhe-2 (KT-2) is a solid-fueled launch vehicle which could be based on the DF-31 missile. Two versions have been proposed:


Kaituozhe-2

The Kaituozhe-2 (KT-2, AKA Kaituo-2) features a possibly DF-31 based stage 1, topped by a small diameter stage 2 and 3. It has reportedly a payload of 800 kg to low earth orbit. The maiden flight of the Kaituozhe-2 took place at 23:45 UTC on March 2, 2017, from
Jiuquan Jiuquan, formerly known as Suzhou, is a prefecture-level city in the northwesternmost part of Gansu Province in the People's Republic of China. It is more than wide from east to west, occupying , although its built-up area is mostly located in i ...
(apparently from one of the two solid rocket launch pads). The rocket placed the
Tiankun-1 Tiankun-1 (also known as TK-1) is a Chinese experimental technology demonstration satellite developed, operated, and launched by China Aerospace Science and Industry Corporation (CASIC). It was launched on March 2, 2017, and is designed in order ...
(TK-1) satellite into polar orbit. The KT-2 is a rapid-response launcher; the rocket is capable of mobile-launch from a transporter-erector-launcher (TEL) vehicle.


Kaituozhe-2A

The Kaituozhe-2A (KT-2A) features a possibly DF-31 based stage 1, augmented by two DF-21 based strap-on boosters. It features a stage 2 with the same diameter as the stage 1 and the same smaller diameter stage 3 as the Kaituozhe-2. It has reportedly a payload of 2000 kg to low earth orbit.


See also

*
Comparison of orbital launchers families This article compares different orbital launcher families (although many launchers that are significantly different from other members of the same 'family' have their own separate entries). The article is organized into two tables: the first tabl ...
*
Comparison of orbital launch systems This comparison of orbital launch systems lists the attributes of all individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or in development as of 2022; a second list includes all retired roc ...
* Kuaizhou launcher *
Long March 6 The Long March 6 () or Chang Zheng 6 as in pinyin, abbreviated LM 6 for export or CZ 6 within China, is a Chinese liquid-fuelled launch vehicle of the Long March family, which was developed by the China Aerospace Science and Technology Corpor ...


References

{{Chinese space program Space launch vehicles of China Vehicles introduced in 2002