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Shanghai Academy of Spaceflight Technology Powered by www.300.cn 沪ICP备15011809号 |
Detail
LM-4B/4C
Long March 4B/4C Launch Vehicle (LM-4B/4C) is three-stage storable liquid propellant launch vehicles with 47m in length and 3.35m in diameter. It is mainly used for SSO, LEO and highly elliptic orbit satellite missions. LM-4B was successfully launched for the first time on May 10th, 1999. LM-4C was successfully launched for the first time on April 27th, 2006.
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1 Payload Fairing 2 Satellite(s) 3 Payload Support Bay 4 3rd Stage Common Base Tank 5 3rd Stage Engines 6 Inter-stage Structure 7 2nd Stage Tank (Oxidizer) 8 Inter-tank Structure 9 2nd Stage Tank (Fuel) 10 2nd Stage Vernier Engines 11 2nd Stage Main Engine 12. Inter-stage Structure 13 1st Stage Tank (Oxidizer) 14 Inter-tank Structure 15 1st Stage Tank (Fuel) 16 Backward Transition Section 17 Tail Section 18 Stabilizing Fin 19 1st Stage Engine |
LM-4B/4C Configuration
Besides single payload missions, LM-4B/4C can also perform multiple-satellite missions and piggyback missions. LM-4B can deliver a 2200kg payload into 700km SSO. LM-4C can deliver a 2800kg payload into 700km SSO.
The standard payload adapter interfaces that LM-4B/4C adopts are Φ660, Φ937, Φ1194, Φ1664 and Φ2000, and LM-4B/4C can also provide Φ300 and SPOD interfaces for piggyback missions.
Payload Fairings and Adapaters
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2 SCs Configuration(A) |
2 SCs Configuration(B) |
3 SCs Configuration |
Multiple-satellite Mission Configuration
Main Characters
|
Parameter |
LM-4B/4C |
|
Length (m) |
46.95 |
|
Lift- off Mass (t) |
250 |
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Lift- off Thrust (kN) |
2961.6 |
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Propellant |
UDMH & N2O4 |
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PLF Diameter (m) |
4.0 / 3.8 / 3.35 / 2.9 |
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Third Stage Diameter (m) |
2.9 |
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Second Stage Diameter (m) |
3.35 |
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First Stage Diameter (m) |
3.35 |
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Mission Oribt |
SSO / LEO |
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Payload Capacity (kg) (600km SSO) |
2910(LM-4B)/3200(LM-4C) |
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The injection accuracy ( 3σ) of typical mission is as follows: - Semi-major axis deviation(△a): ±5km - Orbit eccentricity deviation(△e): ±0.003 - Inclination deviation(△i): ±0.08° - Lead time T0 + 15 months T0 + 6 months for piggybacka |
Record of launch vehicle CZ-4B
|
NO. |
Launch Vehicle |
Time |
Satellites |
Orbit |
|---|---|---|---|---|
|
1 |
CZ-4B_Y2 |
1999-5-10 |
FengYun No.1 meteorological satellite/Practice satellite No.5 |
SSO |
|
2 |
CZ-4B_Y1 |
1999-10-14 |
Resource No.1 Satellite |
SSO |
|
3 |
CZ-4B_Y3 |
2000-9-1 |
Resource Satellite No.2-01 |
SSO |
|
4 |
CZ-4B_Y5 |
2002-5-15 |
FengYun No.1 meteorological satellite |
SSO |
|
5 |
CZ-4B_Y6 |
2002-10-27 |
Resource Satellite No.2-012 |
SSO |
|
6 |
CZ-4B_Y4 |
2003-10-21 |
Resource No.1 Satellite |
SSO |
|
7 |
CZ-4B_Y7 |
2004-9-9 |
Practice No.6-01 Double-Satellite |
SSO |
|
8 |
CZ-4B_Y11 |
2004-11-6 |
Resource Satellite No.2-03 |
SSO |
|
9 |
CZ-4B_Y16 |
2006-10-24 |
Practice No.6-02 Double-Satellite |
SSO |
|
10 |
CZ-4B_Y17 |
2007-9-19 |
Resource Satellite No.1-02B |
SSO |
|
11 |
CZ-4B_Y22 |
2008-10-25 |
Practice No.6-03 Double-Satellite |
SSO |
|
12 |
CZ-4B_Y20 |
2008-12-15 |
remote sensing satellite No.5 |
SSO |
|
13 |
CZ-4B_Y23 |
2010-10-6 |
Practice No.6-04 Double-Satellite |
SSO |
|
14 |
CZ-4B_Y14 |
2011-8-16 |
Ocean exploration satellite |
SSO |
|
15 |
CZ-4B_Y21 |
2011-11-9 |
remote sensing satellite No.12 |
SSO |
|
16 |
CZ-4B_Y15 |
2011-12-22 |
Resource satellite No.1-02C |
SSO |
|
17 |
CZ-4B_Y26 |
2012-1-9 |
Resource satellite No.3, Luxemburg satellite |
SSO |
|
18 |
CZ-4B_Y12 |
2012-5-10 |
remote sensing satellite No.14 |
SSO |
|
19 |
CZ-4B_Y25 |
2013-10-25 |
Prictice satellite No.16 |
LEO |
|
20 |
CZ-4B_Y10 |
2013-12-9 |
Resource Satellite No.1-03 |
SSO |
|
21 |
CZ-4B_Y27 |
2014-8-19 |
Gaofen No.2 satellite |
SSO |
|
22 |
CZ-4B_Y28 |
2014-9-8 |
remote sensing satellite No.21 |
SSO |
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23 |
CZ-4B_Y32 |
2014-12-7 |
Resource Satellite No.1-04 |
SSO |
|
24 |
CZ-4B_Y29 |
2014-12-27 |
remote sensing satellite No.26 |
SSO |
|
25 |
CZ-4B_Y30 |
2015-6-26 |
Gaofen No.8 satellite |
SSO |
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26 |
CZ-4B_Y24 |
2015-11-8 |
remote sensing satellite No.28 |
SSO |
|
27 |
CZ-4B_Y33 |
2016-5-30 |
Resource Satellite No.3-02 |
SSO |
|
28 |
CZ-4B_Y35 |
2016-6-29 |
Prictice satellite No.16-02 |
LEO |
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29 |
CZ-4B_Y31 |
2017-6-15 |
HXMT satellite |
LEO |
Record of launch vehicle CZ-4C
|
NO. |
Launch Vehicle |
Time |
Satellite |
Orbit |
|
1 |
CZ-4C_Y1 |
2006-4-27 |
remote sensing satellite No.1 |
SSO |
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2 |
CZ-4C_Y3 |
2007-11-12 |
remote sensing satellite No.3 |
SSO |
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3 |
CZ-4C_Y2 |
2008-5-27 |
FengYun meteorological satellite No.3-01 |
SSO |
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4 |
CZ-4C_Y4 |
2009-12-15 |
remote sensing satellite No.8 |
SSO |
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5 |
CZ-4C_Y5 |
2010-3-5 |
remote sensing satellite No.9 |
CIO |
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6 |
CZ-4C_Y6 |
2010-8-10 |
remote sensing satellite No.10 |
SSO |
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7 |
CZ-4C_Y7 |
2010-11-5 |
FengYun meteorological satellite No.3-02 |
SSO |
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8 |
CZ-4C_Y10 |
2012-5-29 |
remote sensing satellite No.15 |
SSO |
|
9 |
CZ-4C_Y9 |
2012-11-25 |
remote sensing satellite No.16 |
CIO |
|
10 |
CZ-4C_Y11 |
2013-7-20 |
Innovation satellite No.3/Experimental satellite No.7/Practice satellite No.15 |
SSO |
|
11 |
CZ-4C_Y13 |
2013-9-2 |
remote sensing satellite No.17 |
CIO |
|
12 |
CZ-4C_Y12 |
2013-9-23 |
FengYun meteorological satellite No.3-03 |
SSO |
|
13 |
CZ-4C_Y14 |
2013-11-20 |
remote sensing satellite No.19 |
SSO |
|
14 |
CZ-4C_Y15 |
2014-8-9 |
remote sensing satellite No.20 |
CIO |
|
15 |
CZ-4C_Y16 |
2014-10-20 |
remote sensing satellite No.22 |
SSO |
|
16 |
CZ-4C_Y17 |
2014-12-11 |
remote sensing satellite No.25 |
CIO |
|
17 |
CZ-4C_Y18 |
2015-8-27 |
remote sensing satellite No.27 |
SSO |
|
18 |
CZ-4C_Y8 |
2015-11-27 |
remote sensing satellite No.29 |
SSO |
|
19 |
CZ-4C_Y19 |
2016-8-10 |
Gaofen No.3 satellite |
SSO |
|
20 |
CZ-4C_Y22 |
2016-9-1 |
Gaofen No.10 satellite |
SSO |
|
21 |
CZ-4C_Y21 |
2017-11-15 |
FengYun meteorological satellite No.3-04 |
SSO |