- Long March 3A
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Long March 3A
The launch of Chang'e 1 using a Long March 3A at Xichang Satellite Launch CenterFunction Carrier rocket Manufacturer CALT Country of origin China Size Height 52.52 metres (172.3 ft)[1] Diameter 3.35 metres (11.0 ft)[1] Mass 241,000 kilograms (530,000 lb)[1] Stages 3 Capacity Payload to
GTO2,600 kilograms (5,700 lb)[2] Associated rockets Family Long March Derivatives Long March 3B Launch history Status Active Launch sites LC-2, XSLC Total launches 21[2] Successes 21[2] Maiden flight 8 February 1994[2] The Long March 3A (Chinese: 长征三号甲火箭), also known as the Chang Zheng 3A, CZ-3A and LM-3A, is a Chinese orbital carrier rocket. It is a 3-stage rocket, and is usually used to place communications satellites and Beidou navigation satellites into geosynchronous transfer orbits.
It has formed the basis of the Long March 3B, which is a heavier version with four liquid booster rockets.
Launches
Long March 3A rockets have been launched from Launch Areas 2 and 3 at the Xichang Satellite Launch Centre. Its maiden flight was on 8 February 1994. On 24 October 2007, a Long March 3A launched Chang'e-1, the first Chinese Lunar probe.[citation needed]
The Long March 3A has made 17 consecutive successful launches with an overall perfect launch record.[citation needed]
Technical data
LM-3A is a 3-stage launch vehicle developed on the basis of LM-3 and LM-2C. Its third stage is powered by cryogenic propellants: liquid hydrogen and liquid oxygen. It is dedicated for launching spacecraft into GTO. Its launch capability for GTO mission is 2,600 kg. The fairing static envelope is 3m in diameter.[2]
References
Expendable launch systems Current Ariane 5 · Atlas V · Delta (II · IV) · Dnepr-1 · GSLV · H-IIA · H-IIB · Kaituozhe-1 · Kosmos-3M · Long March (1D · 2C · 2D · 2F · 3A · 3B · 3C · 4B · 4C) · Minotaur (I · IV) · Naro-1 · Paektusan · Pegasus · Proton (K · M) · PSLV · Rokot · Safir · Shavit · Shtil' · Start-1 · Strela · Soyuz (U · FG · 2) · Taurus · Unha · VLS-1 · Volna · Zenit (2 · 2M · 3SL · 3SLB)
Planned Angara · Athena (Ic · IIc) · GSLV III · Haas · Long March (5 · 6 · 7) · Minotaur V · RPS-420 · Rus-M · Soyuz-1 · Simorgh · TSLV · Taurus II · Tsyklon-4 · Vega · Zenit-3F
Previous Ariane (1 · 2 · 3 · 4) · ASLV · Athena (I · II) · Atlas (B · D · E/F · G · H · I · II · III · LV-3B · SLV-3 · Able · Agena · Centaur) · Black Arrow · Caleb · Conestoga · Delta (A · B · C · D · E · G · J · L · M · N · 0100 · 1000 · 2000 · 3000 · 4000 · 5000 · III) · Diamant · Energia · Europa · Falcon 1* · Feng Bao 1 · H-I · H-II · J-I · Juno I · Juno II · Kosmos (1 · 2I · 3) · Lambda (4S) · Long March (1 · 2A · 2E · 3 · 4A) · Mu (4S · 3C · 3H · 3S · 3SII · V) · N1 · N-I · N-II · Pilot · R-7 (Luna · Molniya (M) · Polyot · Soyuz (L · M · U2) · Soyuz/Vostok · Sputnik · Voskhod · Vostok (L · K · 2 · 2M)) · Saturn (I · IB · V · INT-21) · Scout · SLV · Sparta · Thor (Able · Ablestar · Agena · Burner · Delta · DSV-2U) · Thorad-Agena · Titan (II GLV · IIIA · IIIB · IIIC · IIID · IIIE · 34D · 23G · CT-3 · IV) · Tsyklon (2 · 3) · Vanguard
- - Falcon 1 designed for partial reuse, however recovery failed on the first three flights and remaining vehicles were flown expendably
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