N-II (rocket)

Last updated
  1. "JAXA | Engineering Test Satellite IV "KIKU-3" (ETS-IV)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  2. 1 2 "JAXA | Geostationary Meteorological Satellite "Himawari" (GMS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  3. 1 2 "JAXA | Communication Satellite "Sakura" (CS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  4. 1 2 "JAXA | Broadcasting Satellite "Yuri" (BS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
  5. "JAXA | Marine Observation Satellite-1 "Momo-1" (MOS-1)". JAXA | Japan Aerospace Exploration Agency. Retrieved 2020-03-16.
N-II.svg
The N-II rocket
Function Carrier rocket
Manufacturer McDonnell Douglas (design)
Mitsubishi Heavy Industries (production)
Country of originUnited States (design)
Japan (production)
Size
Height35 metres (115 ft)
Diameter2.44 metres (8.0 ft)
Mass132,690 kilograms (292,530 lb)
Stages2 or 3
Capacity
Payload to LEO
Mass2,000 kilograms (4,400 lb)