N-I (rocket)

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N2O4  / A-50
  1. 1 2 3 4 5 Wade, Mark. "Delta". Encyclopedia Astronautica. Archived from the original on 17 August 2013. Retrieved 3 September 2008.
  2. 1 2 "JAXA Digital Archives". Japan Aerospace Exploration Agency. Archived from the original on 9 September 2009. Retrieved 1 October 2009.
  3. ↑ "N-Iロケット開発の歩み". Yukihiko Takenaka, NASDA. Retrieved 10 February 2011.
  4. ↑ "三菱重工 名古屋誘導推進システム製作所 事業所紹介 沿革". Mitsubishi Heavy Industries. Archived from the original on 4 July 2011. Retrieved 10 February 2011.
  5. ↑ "第1部 創造性豊かな科学技術を求めて 第2章 自主技術開発への展開 第3節 先導的・基盤的科学技術分野における自主技術開発の展開 2.宇宙開発". Ministry of Education, Culture, Sports, Science and Technology. Archived from the original on 15 June 2008. Retrieved 10 February 2011.
  6. ↑ Krebs, Gunter. "N-1". Gunter's Space Page. Retrieved 31 August 2008.
  7. ↑ Pearlman, Robert (29 February 2016). "Space Station Command Change Is One Giant Leap (Day) for Space History". Space.com . Retrieved 2 November 2017.
  8. ↑ "JAXA | N-I Launch Vehicle". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  9. 1 2 3 4 5 6 7 McDowell, Jonathan. "Thor". Orbital and Suborbital Launch Database. Jonathan's Space Report. Archived from the original on 1 August 2020. Retrieved 31 August 2008.
  10. 1 2 "JAXA | Engineering Test Satellite I "KIKU-1" (ETS-I)". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  11. 1 2 3 "JAXA | Ionosphere Sounding Satellite "UME" (ISS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  12. 1 2 "JAXA | Engineering Test Satellite II "KIKU-2" (ETS-II)". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  13. 1 2 3 "JAXA | Experimental Communications Satellites "Ayame" (ECS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  14. 1 2 "JAXA | Engineering Test Satellite III "KIKU-4" (ETS-III)". JAXA | Japan Aerospace Exploration Agency. Retrieved 18 February 2024.
  15. ↑ "ISS a, b (Ume 1, 2)". Gunter's Space Page. Retrieved 18 February 2024.
N-I
N-I.svg
The N-I rocket [1]
Function Small-lift launch vehicle
Manufacturer McDonnell Douglas (design)
Mitsubishi Heavy Industries (production)
Country of originUnited States (design)
Japan (production)
Size
Height34 m (112 ft) [1]
Diameter2.44 m (8.0 ft)
Mass131,330 kg (289,530 lb) [1]
Stages2 or 3
Capacity
Payload to LEO
Mass1,200 kg (2,600 lb) [1]