1985-056A
Giotto was based on the Geos bus and built by the same BAe/STAR consortium. The probe was built from the Geos engineering model. ESA controlled Giotto from ESOC. Flyby velocity was 68.4 km/s with 596 km closest approach.
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| Giotto |
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| Date | Time | Event | Orbit |
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| 1985 Jul 2 | 1123:13 | Launch by Ariane I | CSG |
| | | T+2:25 St 1 MECO |
| | | T+2:30 Stage 2 burn |
| | | T+4:14 Fairing |
| | | T+4:51? St 2 sep |
| | | T+4:55? Stage 3 burn 9:21? |
| | 1137 | T+14:16? Stage 3 MECO |
| | 1138? | Stage 3 sep | 203 x 35421 x 7.0 |
| | 1139 | Perigee |
| | 1145 | AOS by Malindi |
| | 1650 | Spin axis slew |
| 1985 Jul 2 | 1700? | Apogee 1 |
| 1985 Jul 2 | 2110 | Perigee 1, 202 km |
| | 2210 | Perigee 1 from TLE |
| 1985 Jul 3 | 0230? | Apogee 2 |
| | 0844 | Perigee 2 from TLE |
| | 1400? | Apogee 2 |
| | | Spinup |
| | 1914 | Perigee 3 from TLE 2 |
| | 1918 | Perigee 3 from TLE 1 |
| | 1923:47 | Mage 1S perigee burn 1.40km/s | Solar orbit |
| 1924:42 | Burnout (55s) |
| 1985 Jul 4 | 0333? | Pass EL1:4 |
| 1985 Jul 4 | 0730 | Nozzle cover closed |
| 1985 Jul 6 | 0947 | HGA release |
| | | Begin cruise, mass 578.5 kg |
| 1985 Jul 8 | 0230? | Pass L1 |
| 1985 Jul 15 | | 3.43Mkm range |
| 1985 Aug 26 | | TCM-1, 7.27m/s, 92 min |
| 1985 Oct 2 | | Range 20.235Mkm to Earth |
| 1986 Jan 24 | | Antenna lock loss, recovered by DSN |
| 1986 Mar 12 | 0053 | TCM 2.5m/s |
| | 0125 | TCM complete |
| 1986 Mar 13 | 1816 | (ERT) PKS gets signal |
| 1986 Mar 13 | | Encounter P/Halley at 0.90AU, vrel 68.4 km/s |
| | | Mass 573.9 kg |
| | 2356:58 | First bumper shield penetration |
| 1986 Mar 14 | 0002:52 | Last image |
| | 0002:52 | Hit by 1g of particles |
| | 0002:55 | Loss of signal |
| 1986 Mar 14 | 0003:02 | Passed 596 km from nucleus |
| | 0003:19 | Signal recovered |
| | 0004:34 | Spacecraft nutating |
| | 0034:58 | Spacecraft recovered |
| 1986 Mar 19 | | TCM 4h30m, 63 m/s, 19 kg |
| 1986 Mar 20 | | TCM 4:10min, 46m/s, 14 kg |
| 1986 Mar 21 | | TCM 16min, 2.6m/s, 1 kg | 0.833 yr 0.733 x 1.04 AU |
| 1986 Apr 1 | | TCM 1.5m/s |
| 1986 Apr 2 | | TCM 1.3m/s? |
| 1986 Apr 2 | 0225 | Deactivated |
| 1990 Feb 20 | | Reactivated by DSN/Madrid, R=102.9 Mkm Rdot=14.54km/s Vsun=37.36km/s |
| 1990 Feb 21 | | HGA despin attempts |
| 1990 Feb 25 | 1745 | ESOC resumes control |
| | | HMC and NMS deactivates |
| 1990 Mar 3 | | Perihelion |
| 1990 Mar 13 | | TCM to retarget for Grigg-Skjellerup |
| 1990 Jul 2 | 1001:18 | Flyby Earth, 22730 km over Australia | 390d? |
| | | Inc = 45 deg |
| 1990 Jul 16 | | TCM 0.5m/s |
| 1990 Jul 22 | | Hibernation mode |
| 1992 Apr | | Reactivated |
| 1992 May 22 | | TCM, 3.5m/s targeting to 800 km |
| 1992 Jul 1 | | Science instruments on |
| 1992 Jul 8 | | TCM, 2m/s targeting to 200 km |
| 1992 Jul 10 | 1519 | Encounter P/Grigg-Skjellerup 200 km, at 1.01 AU from Sun LT=24min |
| | | Rel 13.99 km/s |
| 1992 Jul 11 | | Experiments off |
| 1992 Jul 21 | | TCM, target to Earth swingby, 4h burn 33m/s |
| 1992 Jul 23 | | TCM correction 3m/s |
| 1992 Jul 23 | | In hibernation mode
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