Kounotori 8 (こうのとり8号機), also known as HTV-8 was the 8th flight of the H-II Transfer Vehicle, a robotic cargo spacecraft to resupply the International Space Station. It was launched on 24 September 2019, 16:05:05 UTC.[8]
H-II Transfer Vehicle (HTV-8) being grappled by the Canadarm2 on 1 November 2019. | |
| Mission type | ISS resupply |
|---|---|
| Operator | JAXA |
| COSPAR ID | 2019-062A |
| SATCAT no. | 44546 |
| Mission duration | 40 days |
| Spacecraft properties | |
| Spacecraft | Kounotori 8 |
| Spacecraft type | HTV |
| Manufacturer | Mitsubishi Heavy Industries |
| Launch mass | 15800 kg [1] |
| Dry mass | 10500 kg |
| Payload mass | 5300 kg |
| Dimensions | 9.8 metre of long, 4.4 metre of diameter |
| Start of mission | |
| Launch date | 24 September 2019, 16:05:05 UTC[2] |
| Rocket | H-IIB No. 8 |
| Launch site | Tanegashima, Yoshinobu-2 |
| Contractor | Mitsubishi Heavy Industries |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 3 November 2019 |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Low Earth orbit |
| Inclination | 51.66° |
| Berthing at ISS | |
| Berthing port | Harmony nadir |
| RMS capture | 28 September 2019, 11:12 UTC [3] |
| Berthing date | 28 September 2019, 14:09 UTC [4] |
| Unberthing date | 1 November 2019, 13:45 UTC [5] |
| RMS release | 1 November 2019, 17:21 UTC [6][7] |
| Time berthed | 34 days |
| Cargo | |
| Mass | 5300 kg |
| Pressurised | 3400 kg |
| Unpressurised | 1900 kg |
HTV ISS Resupply | |
Major changes from previous Kounotori are:[9]
Kounotori 8 carries about 5300 kg of cargo, consisting of 3400 kg in the pressurized compartment and 1900 kg in the unpressurized compartment.[9]
Cargo in the Pressurized Logistics Carrier (PLC) include:[9]
In the Unpressurized Logistics Carrier (ULC), Kounotori 8 carries six lithium-ion batteries Orbital Replacement Units (ORUs) for replacing the ISS's existing nickel-hydrogen batteries. The transportation of replacement batteries is a continuation from the previous Kounotori 6 and 7, and will continue through to Kounotori 9.[9]
The H-IIB launch vehicle carrying Kounotori 8 was initially scheduled to be launched at 21:33:29 UTC, 10 September 2019.[11][12] During launch preparation, a fire broke out at the launch pad at around 18:05 UTC (T minus 3.5 hours), and the launch was called off.[13] The cause of fire was attributed to the static electricity on the heat resistant material under the mixture of liquid oxygen and gas oxygen for the engine pre-cooling.[14]
After the modification to the mobile launch platform to suppress static electricity, a new launch was scheduled at 23 September 2019, 16:30 UTC,[14] but the collision avoidance check revealed that the 2nd stage of the launch vehicle might approach near the Soyuz MS-15 which was scheduled to be launched on 25 September 2019. A revised launch schedule was set for 16:05 UTC, 24 September 2019.[15] On 24 September 2019, 16:05:05 UTC, the Kounotori 8 aboard H-IIB was launched successfully.[8]
Kounotori 8 was captured by the Space Station Remote Manipulator System (SSRMS) at 23:13 UTC, on 27 September 2019,[16] and berthed at Harmony's nadir Common Berthing Mechanism (CBM) by 17:55 UTC, on 28 September 2019.[17]
The External Palette (EP8), which carries the lithium-ion battery Orbital Replacement Units (ORU), was extracted from the Kounotori 8's Unpressurized Logistics Carrier (ULC) by the SSRMS (Canadarm2) on 29 September 2019.[18]
The External Palette of Kounotori 7 (EP7) was placed in the Kounotori 8's ULC.[19] EP7 was left on the ISS after the departure of Kounotori 7 due to the schedule change of extravehicular activity after the launch failure of Soyuz MS-10.
On 1 November 2019, Kounotori 8 was detached from Harmony's CBM by the SSRMS (Canadarm2), and it was released into orbit at 17:20 UTC.[20]
It was disposed by the destructive reentry to the Earth atmosphere at around 02:09 UTC, on 3 November 2019.[21]
Kounotori H-II Transfer Vehicle spaceflights | ||
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| See also |
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Uncrewed spaceflights to the International Space Station | ||
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in brackets). | |