TopicsTD1-L08E1 operation schedule

Our first touchdown (TD) operation will be performed from February 20 – 22, 2019. As the touchdown site on asteroid Ryugu is named L08-E1, this operation has the name TD1-L08E1.

Main Schedule for the TD1-L08E1 operation

Note: This is an updated schedule following the delay at the beginning of the descent, resulting in a change from the initial plan.

Date & Time UTC
( ) is the ground confirmation time
Date & Time JST
( ) is the ground confirmation time
Spacecraft line-of-sight velocity (cm/s) Altitude (m) Event
2019/2/20 21:30
→05:30
2019/2/21 6:30
→14:30
Shift 1  [Start descent]
2019/2/20 22:00
→ 05:55
2019/2/21 7:00
→ 14:55
Communication via Usuda Deep Space Center begins
2019/2/20 22:00
→ 07:05
2019/2/21 7:00
→ 16:05
Communication via Canberra DSN begins
2019/2/21 3:132019/2/21 12:13Gate 1: begin vertification (telemetry check before the start of the descent)
2019/2/21 4:13
(02/21 4:32)
2019/2/21 13:13
(02/21 13:32)
-9020,000Begin descent
2019/2/21 5:00
→ 13:00
2019/2/21 14:00
→ 22:00
Shift 2 [Descent deceleration]
2019/2/21 6:55
→ 15:00
2019/2/21 15:55
→ 24:00
Communication via Madrid DSN begins
2019/2/21 9:33
(02/21 09:52)
2019/2/21 18:33
(02/21 18:52)
-104,500Decelerate descent speed ΔV
2019/2/21 9:522019/2/21 18:52Gate 2: begin vertification (confirm descent deceleration ΔV)
2019/2/21 12:30
→ 20:30
2019/2/21 21:30
→ 05:30
Shift 3 [Monitor]
2019/2/21 14:55
→ 22:05
2019/2/21 23:55
→ 07:05
Communication via Goldstone DSN begins
2019/2/21 18:06
(02/21 18:25)
2019/2/22 3:06
(02/22 03:25)
1,500
2019/2/21 19:29
(02/21 19:48)
2019/2/22 4:29
(02/22 04:48)
1,000
2019/2/21 20:00
→ 04:30
2019/2/22 5:00
→ 13:30
Shift 4 [Go/NoGo]
2019/2/21 19:40
→ 07:05
2019/2/22 4:40
→ 16:05
Comm. via Canberra begins
2019/2/21 20:36
(02/21 20:55)
2019/2/22 5:36
(02/22 05:55)
500
2019/2/21 21:022019/2/22 6:02Gate3: begin vertification (Go/NoGo judgement)
2019/2/21 21:30
→ 05:55
2019/2/22 6:30
→ 14:55
Comm. via Usuda beings
2019/2/21 21:33
(02/21 21:52)
2019/2/22 6:33
(02/22 06:52)
250
2019/2/21 22:08
(02/21 22:27)
2019/2/22 7:08
(02/22 07:27)
45Begin hovering, switch to LGA
2019/2/21 23:06
(02/21 23:25)
2019/2/22 8:06
(02/22 08:25)
00Touchdown
2019/2/21 23:06
(02/21 23:25)
2019/2/22 8:06
(02/22 08:25)
45.5Surface withdrawal, Ascent ΔV
2019/2/21 23:252019/2/22 8:25500Gate4: begin vertification (withdrawal, confirm increase in ΔV )
2019/2/21 23:442019/2/22 8:441,000Gate5: begin vertification (health check)
2019/2/22 2:08
(02/22 02:27)
2019/2/22 11:08
(02/22 11:27)
44.55,000Reduce rate of ascent ΔV
2019/2/22 4:00
→ 12:00
2019/2/22 13:00
→ 21:00
Shift 5 [Return to HP]
2019/2/22 6:55
→ 15:00
2019/2/22 15:55
→ 24:00
Comm. via Madrid begins
2019/2/22 9:372019/2/22 18:3717,000Gate 6: begin vertification
2019/2/22 10:182019/2/22 19:18TBDIncrease ΔV to return to HP
2019/2/22 11:262019/2/22 20:26Cancel spacecraft descent configuration
~2019/2/27~2019/2/27Return to home position
Notes:
  • Time: Approximate scheduled time. UTC is Universal Time, JST is Japan standard time. There is a possibility that this may change during operation.
  • Spacecraft speed: This is the speed along the line-of-sight relative to the asteroid (minus is towards the asteroid, positive is away). Numerical value is displayed only when speed control is performed. After a speed control operation, the speed changes due to the gravitational force of Ryugu and other celestial bodies.
  • Altitude: Approximate distance from the surface of Ryugu

Schematic of the TD1-L08E1 operation
TD1-L08E1 low altitude sequence

Hayabusa2 project
2019.02.21