2016-042A
Referred to as Reduced-Scale Cabin. (Suo bi fanhui cang)
\uni{ 缩比返回舱}{ }
or\uni{ 多用途飞船返回舱飞行试验任务 }{ }
Duo yongtu feichuan fanhui cang feixing shiyan renwu Multipurpose return capsule spacecraft flight test mission or simply\uni{ 多用途飞船缩比返回舱}{ }
Duo yongtu feichuan fanhui cangMultipurpose subscale return capsule, developed by CAST. 2.3m high 1.6 to 2.6m dia truncated cone, 2600 kg.
It included an attached
\uni{ 配重支架}{ }
Pei Zhong zhijia, ballast frame Launch used YZ-1A\uni{ 远征-1Aupper }{ }
stage. Total payload mass 12000 kg.Due to land at 0600 UTC Jun 26 at Dongfeng landing field.
| DFFC | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2016 Jun 25 | 1200:03 | Ignition | |
| 1200:07 | Launch by CZ-7 Y1 | Wenchang LC201 | |
| 1203:01 | T+2:47 or 2:54 Strapons sep | ||
| 1203:17 | T+3:02 or 3:10 Core sep | ||
| T+3:31 or 3:33 Fairing sep | |||
| 1203:19 | Stage 2 burn | ||
| 1209:55 | T+9:52 St 2 MECO | 200 x 394 | |
| 1210 | Sep motor covers | ||
| 1210:02 | T+9:59 YZ-1 separation | 200 x 379 x 40.8 | |
| Ballast support structure separation | |||
| 1214 | C and G close (34 km) | ||
| 1223 | A/B and G 140 km apart | ||
| 1238 | ADRV (AoLong-1) separation | 286 x 376 x 40.8 | |
| 1240? | ADRV adapter separation | ||
| 1255? | YZ-1A burn 1 | ||
| 1342 | Aoxiang Zhixing sep | ||
| YZ-1A burn 2, circular orbit | |||
| BPV sep (Tiange 1 and 2) | 280 x 290 x 40.8 | ||
| 2016 Jun 26 | 0731? | YZ-1A burn 3, DFFC Deorbit 300? x 170 | |
| Ballast separation | |||
| 0732? | YZ1 sep 300? x 130 | ||
| 0732? | YZ-1A burn 4, reorbit 400 x 400? | ||
| 0733? | Entry | ||
| 0736 | Drogues deployed | ||
| 0736 | Main parachute deployed | ||
| 0741 | Landing | ||
| YZ-1A burns | |||
| 2016 Jun 27 | 0700? | YZ-1A deorbit | |
| 0725? | YZ-1A entry over Pacific | ||
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