N-II (rocket)

Last updated
HNO3 /UDMH
  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 m (114 ft 10 in)
Diameter2.44 m (8 ft 0 in)
Mass132,690 kg (292,530 lb)
Stages2 or 3
Capacity
Payload to LEO
Mass2,000 kg (4,400 lb)