Dragonfly (spacecraft): Difference between revisions
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| manufacturer = {{plainlist| | | manufacturer = {{plainlist| | ||
*[[Daobac Space Corporation]] | *[[Daobac Space Corporation]] | ||
*[[Mach Aerospace]] | *[[Mach Aerospace]] | ||
*[[YAT program|YAT 250 - Cihuacoatl]] | *[[Tran International|Tran Heavy Industries]] | ||
*[[YAT program|YAT 250 - Cihuacoatl]] | |||
}} | }} | ||
| designer = | | designer = | ||
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*{{flag|Zacapican}} | *{{flag|Zacapican}} | ||
}} | }} | ||
| operator = {{flagicon_image|AMOS_Flag.png}} [[International Aeronautical Union]] | | operator = {{flagicon_image|AMOS_Flag.png}} [[International Aeronautical Union|IAU]] | ||
| applications = Crewed orbital launch and reentry | | applications = Crewed orbital launch and reentry | ||
| website = | | website = | ||
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<!--Specifications--> | <!--Specifications--> | ||
| spacecraft_type = | | spacecraft_type = {{wp|Reusable launch vehicle|Reusable}} | ||
| spacecraft_bus = | | spacecraft_bus = | ||
| constellation = | | constellation = | ||
| design_life = | | design_life = | ||
| launch_mass = | | launch_mass = {{convert|42,000|kg|lb|abbr=on}} | ||
| dry_mass = | | dry_mass = {{convert|33,000|kg|lb|abbr=on}} | ||
| payload_capacity = | | payload_capacity = {{convert|30,000|kg|lb|abbr=on}} | ||
| crew_capacity = | | crew_capacity = 10 | ||
| volume = | | volume = | ||
| power = | | power = | ||
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<!--Dimensions--> | <!--Dimensions--> | ||
| length = | | length = | ||
| height = | | height = 25 | ||
| diameter = | | diameter = 25 | ||
| width = | | width = | ||
| winged = | | winged = | ||
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<!--Production--> | <!--Production--> | ||
| status = | | status = Active | ||
| planned = | | planned = TBD | ||
| orders = | | orders = TBD | ||
| built = | | built = TBD | ||
| launched = | | launched = TBD | ||
| operational = | | operational = TBD | ||
| retired = | | retired = TBD | ||
| failed = | | failed = TBD | ||
| lost = | | lost = TBD | ||
| maidenlaunch = | | maidenlaunch = | ||
| lastlaunch = | | lastlaunch = | ||
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| next = | | next = | ||
}} | }} | ||
'''Dragonfly''' ({{wp|Malagasy|Nylele}}: ''Angidina'') is {{wp|Reusable launch vehicle|partially reusable}} {{wp|spacecraft}} that can carry both crew and cargo into orbit. The design & operation of the spacecraft is overseen by the [[International Aeronautical Union]], an independent agency of the [[Association of Ozeros Nations]] though the two primary users of the Dragonfly are the [[Daobac Space Corporation]] and [[United Space Exploration Authority]] whereas components of the Dragonly were manufactured by the [[Daobac Space Corporation]], [[Mach Aerospace]], [[Tran International|Tran Heavy Industries]] and [[YAT program|YAT 250 - Cihuacoatl]]. The project began in 1975 |
Latest revision as of 07:43, 8 September 2023
Manufacturer | |
---|---|
Country of origin | |
Operator | IAU |
Applications | Crewed orbital launch and reentry |
Specifications | |
Spacecraft type | Reusable |
Launch mass | 42,000 kg (93,000 lb) |
Dry mass | 33,000 kg (73,000 lb) |
Payload capacity | 30,000 kg (66,000 lb) |
Crew capacity | 10 |
Production | |
Status | Active |
Built | TBD |
On order | TBD |
Launched | TBD |
Operational | TBD |
Retired | TBD |
Failed | TBD |
Lost | TBD |
Dragonfly (Nylele: Angidina) is partially reusable spacecraft that can carry both crew and cargo into orbit. The design & operation of the spacecraft is overseen by the International Aeronautical Union, an independent agency of the Association of Ozeros Nations though the two primary users of the Dragonfly are the Daobac Space Corporation and United Space Exploration Authority whereas components of the Dragonly were manufactured by the Daobac Space Corporation, Mach Aerospace, Tran Heavy Industries and YAT 250 - Cihuacoatl. The project began in 1975