Sigma 5: Difference between revisions
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| SATCAT = CSM: 13106<br>LM: 13108 | | SATCAT = CSM: 13106<br>LM: 13108 | ||
| mission_duration = 11 days, 3 hour, 46 minutes, 2 seconds | | mission_duration = 11 days, 3 hour, 46 minutes, 2 seconds | ||
| spacecraft = {{Unbulleted list | | spacecraft = {{Unbulleted list | ||
|Sigma CSM-137 | |Sigma CSM-137 | ||
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|LM: [[MAOA]]/Albatross | |LM: [[MAOA]]/Albatross | ||
}} | }} | ||
| launch_mass = {{convert| | | launch_mass = {{convert|10869|lb|kg}} | ||
| landing_mass = {{convert| | | landing_mass = {{convert|12054|lb|kg}} | ||
| launch_date = {{start-date|May 2, 1980, 12:10:00|timezone=yes}} UTC | |||
| launch_date = {{start-date|May 2, 1980, | |||
| launch_rocket = {{wp|N1 (rocket)|Atlant-3}} AT-388 | | launch_rocket = {{wp|N1 (rocket)|Atlant-3}} AT-388 | ||
| launch_site = TBD | | launch_site = TBD | ||
| landing_date = {{end-date|May 13, 1980, 18:56:11|timezone=yes}} UTC | |||
| landing_date = {{end-date|May 13, 1980, | |||
| landing_site = TBD | | landing_site = TBD | ||
| recovery_by = [[CRS Wagemut|CRS ''Wagemut'']] | | recovery_by = [[CRS Wagemut|CRS ''Wagemut'']] | ||
| orbit_epoch = 1980, 00:00 UTC | | orbit_epoch = 1980, 00:00 UTC | ||
| orbit_reference = {{wp|selenocentric orbit|Selenocentric}} | | orbit_reference = {{wp|selenocentric orbit|Selenocentric}} | ||
| orbit_periapsis = {{convert| | | orbit_periapsis = {{convert|11.2|nmi|km|order=flip|sp=us}} | ||
| orbit_apoapsis = {{convert| | | orbit_apoapsis = {{convert|56.9|nmi|km|order=flip|sp=us}} | ||
| orbit_inclination = | | orbit_inclination = | ||
| orbit_period = | | orbit_period = 1.89 hours | ||
| apsis = selene | | apsis = selene | ||
|interplanetary = | |interplanetary = | ||
<!--Cargo parameters--> | <!--Cargo parameters--> | ||
| payload_items = {{Unbulleted list | | payload_items = {{Unbulleted list | ||
Line 49: | Line 44: | ||
}} | }} | ||
| instruments = <!--a list of instruments on the satellite--> | | instruments = <!--a list of instruments on the satellite--> | ||
| docking = | | docking = | ||
| crew_size = 4 | | crew_size = 4 | ||
| crew_members = {{Unbulleted list | | crew_members = {{Unbulleted list | ||
Line 73: | Line 52: | ||
|Aleksandr Sahalinov | |Aleksandr Sahalinov | ||
}} | }} | ||
| crew_EVAs = 1 in [[cislunar space]] to retrieve film cassettes | | crew_EVAs = 1 in [[cislunar space]] to retrieve film cassettes amd 3 on the lunar surface | ||
| crew_EVA_duration = 1 h 23 min 42 s | | crew_EVA_duration = 1 h 23 min 42 s <small>(spacewalk)</small> | ||
| crew_callsign = {{Unbulleted list | | crew_callsign = {{Unbulleted list | ||
|CSM: ''TBD'' | |CSM: ''TBD'' | ||
|LM: ''Einigung'' | |LM: ''Einigung'' | ||
}} | }} | ||
| crew_photo = [[File:Sigma 5 crew portrait.png|250px]] | | crew_photo = [[File:Sigma 5 crew portrait.png|250px]] | ||
| crew_photo_caption = Left to right: [[Lukas Brennzer]], Georgy Cheryomushev, Walther Gählen, Aleksandr Sahalinov | | crew_photo_caption = Left to right: [[Lukas Brennzer]], Georgy Cheryomushev, Walther Gählen, Aleksandr Sahalinov | ||
| previous_mission = Sigma 4 | | previous_mission = Sigma 4 | ||
| next_mission = Sigma 6 | | next_mission = Sigma 6 |
Revision as of 12:32, 16 April 2020
Mission type | Crewed lunar landing |
---|---|
Operator | MAOA People's Republic of Dulebia space program |
COSPAR ID | CSM: 1980-023A LM: 1980-023B |
SATCAT no. | CSM: 13106 LM: 13108 |
Mission duration | 11 days, 3 hour, 46 minutes, 2 seconds |
Spacecraft properties | |
Spacecraft |
|
Manufacturer |
|
Launch mass | 10,869 pounds (4,930 kg) |
Landing mass | 12,054 pounds (5,468 kg) |
Crew | |
Crew size | 4 |
Members |
|
Callsign |
|
EVAs | 1 in cislunar space to retrieve film cassettes amd 3 on the lunar surface |
EVA duration | 1 h 23 min 42 s (spacewalk) |
Start of mission | |
Launch date | May 2, 1980, 12:10:00 | UTC
Rocket | Atlant-3 AT-388 |
Launch site | TBD |
End of mission | |
Recovered by | CRS Wagemut |
Landing date | May 13, 1980, 18:56:11 | UTC
Landing site | TBD |
Orbital parameters | |
Reference system | Selenocentric |
Periselene altitude | 20.7 kilometers (11.2 nmi) |
Aposelene altitude | 105.4 kilometers (56.9 nmi) |
Period | 1.89 hours |
Epoch | 1980, 00:00 UTC |
Payload | |
Mass |
|
Left to right: Lukas Brennzer, Georgy Cheryomushev, Walther Gählen, Aleksandr Sahalinov |