2013-070A
Lander and rover. Chang'e san hao
\uni{ 嫦娥三号 }{ }
Rover is\uni{ 玉兔}{ }
(Yutu, Jade Rabbit) or\uni{ 玉兔号}{ }
(yutu hao)LV is
\uni{ 长征三号乙改进型火箭 }{ }
(CZ-3BE, Changzheng sanhao yi gaijin [improved] xing huojian [rocket])Chang'E 3 ca. 2012 or later. (Yihua Yan, NAO Beijing) Lander and rover with 30 km range. WIll carry two astro expts: a small photometric telescope for stellar variability studies and a pair of VLF astronomy antennas (1 on lander, 1 on rover)
The LUT observed galaxy M101 in 2015 Jan as part of an international collaboration.
Lander is box + 4 legs + 2 stubby panels. 2.5 x 2.5, 4.8m span across legs. Mass 3800 kg, landing mass 1700 kg? 140 kg rover deployed on ladders, box + 2 panels + 6 wheels
Landing site is called Guang Han Gong (Moon Palace).
| CE3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Dec 1 | 1730:00 | Launch by CZ-3B | XSC |
| T+2:21 Booster sep | |||
| T+2:39 St 1 sep | |||
| T+3:55 Fairing sep | |||
| 1735 | T+5:44 St 2 sep | ||
| 1740 | T+9:56? Stage 3 MECO | ||
| 1743 | T+13:49? Stage 3 MES-2 250 km | ||
| 1747 | T+17:25s? Stage 3 MECO-2 10.87 km/s | ||
| 1748:59 | T+19:00 Stage 3 sep | 210.3 x 389109.2 x 28.5 | |
| 1750 | T+20:50 Probe thruster burn | ||
| Stage 3 retro burn | |||
| 1815 | Landing legs deployed | ||
| 1819 | Solar panels deplpyed | ||
2013 Dec 2 | 0928 | Pass EL1:4 | |
| MC-1 | |||
| MC-2 | |||
| MC-3 | |||
| 2013 Dec 5 | 1741 | Stage 3 enter L sphere | |
| 2013 Dec 6 | 0950 | LOI | 100 x 100 x 90 |
| 1116 | Stage 3 lunar flyby | 3005 x -19346 x 22.61 | |
| 106240 x 662600 x 35.79 | |||
| 2013 Dec 7 | 0452 | Stage 3 depart L sphere | |
| 2013 Dec 10 | 1320 | LOI-2 3 min | 15 x 100 x 90 |
| 2013 Dec 14 | 1259:52 | Descent burn | 14 x 99 x 90 |
| Hover | |||
| 1311:18 | Landing 19.51W 44.12N | ||
| 19.5014W 44.1260N per NSF | |||
| 43 km S of Laplace F, Mare Imbrium | |||
| 2013 Dec 14 | 1728 | Ramp photos | |
| 1910 | Rover on transfer system | ||
| 2006 | Ramp deployed | ||
| 2035 | Yutu rover on surface | ||
| 2013 Dec 23 | 0900? | Rover robot arm deploy | |
| 2015 Sep 17 | 2115 | Stage 3 lunar pass 10127 km | |
Payload:
- 150N thruster + 10N RCS. 1.5-7.5 kN
- MastCam -(Inst. of Optics and Electronics, CAS)
- Descent Camera (BISME, CAST)
- LUT Lunar UV Telescope- NAO China, CAS
- EUV EUV imager - CIOMP-CAS (Changchun Institute of Optics, Fine Mechanics and Physics)
Payload:
- PanCam - Xian Inst of Optics and Prec.Mechanics (CAS)
- GPM Ground penetrating radar, Inst of Electronics (CAS)
- VNIS Vis/NIR imaging spectrometer, SITP (Shanghai Institute of Technical Physics, CAS)
- APXS Institute of High Energy Physics (IHEP), CAS
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