M-5 (8)

Last modification: March 9, 2006


M-5

    Launch date
 Launch window:
 Status:
 February 21, 2006 - 2128 UTC.
 Completed
.
 Launch site
 Location:
 Launch complex:
 Kagoshima Space Centre (Japan)
 Uchinoura Launch Complex
 Launch vehicle

 Version:
 Upper stage:
 Payload fairing:
 Launch vehicle prime:
 Launch provider:
 Flight number:

 M-5 Upgrade
 [M-34 3rd stage]
 Standard
 IHI Aerospace
 Japan Aerospace Exploration Agency (JAXA)
 N°8
 Performance
 Targeted orbit:
 Overall lift-off mass:
 Total payload mass:
 Sun-Synchronous Orbit
 
About 140,000 kg
 About 1,050 kg (est.
)
 Milestones
 Delayed from Feb. 18 due to range conflict with H-2A (F9).
 Delayed from Feb. 20 due to weather.

 

Payload
 Payload designation Launch customer
Launch contract
Launch mass
Launch adapter
  Astro F JAXA
n.s.
960 kg
  n.a.
  CUTE-1.7 Tokyo Institute of Technology
n.a.
3 kg
  n.a.
  SSP JAXA?
n.a.
n.a.
  n.a.

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