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Table 3

Trajectory-correction schedule for the orbiting of SRG near the L2 point.

No. Date/time Days in flight Number of PU ignitions Total characteristic speed Consumed propellant
(Moscow) m s−1 kg
1 Oct. 21, 2019 100 1 0.21 0.25
19:00:00.000
2 Dec. 10, 2019 150 1 0.18 0.21
19:00:00.000
3 Jan. 30, 2020 201 1 0.27 0.32
19:00:00.000
4 Apr. 01,2020 263 1 1.00 1.13
19:00:00.000
5 Jun. 16, 2020 339 1 0.95 1.07
21:00:00.000
6 Aug. 05, 2020 389 1 0.94 1.08
20:00:00.000
7 Oct. 05, 2020 450 1 3.01 3.38
19:00:00.000
8 Nov. 23, 2020 499 1 6.23 6.99
19:00:00.000
9 Feb. 28, 2020 588 1 6.24 6.94
17:00:00.000

Remaining propellant: 319.63 kg

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