N-I (rocket)

This article is about the Japanese rocket. For the Soviet rocket, see N1 rocket.

N-I

The N-I rocket
Function	Carrier rocket
Manufacturer	Mitsubishi Heavy Industries
Country of origin	USA (design) Japan (production)
Size
Height	34 metres (112 ft)
Diameter	2.44 metres (8.0 ft)
Mass	131,330 kilograms (289,530 lb)
Stages	2 or 3
Capacity
Associated rockets
Family	Delta
Launch history
Status	Retired
Launch sites	LA-N, Tanegashima
Total launches	7
Successes	6
Partial failures	1
First flight	9 September 1975
Last flight	3 September 1982

Mock up of N-1

The N-I or N-1 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II. Six of the seven launches were successful, however on the fifth flight, there was recontact between the satellite and the third stage, which caused the satellite to fail.

On 29 February 1976, the second N-I conducted the only orbital launch to occur on a leap day (as of year 2008).

Launch history

Date/Time (GMT)	S/N	Payload	Orbit	Remarks
9 September 1975, 05:30	1(F)	ETS-1 (JETS-1/Kiku-1)	LEO
29 February 1976, 03:30	2(F)	ISS-1 (JISS-1/Ume-1)	LEO
23 February 1977, 08:50	3(F)	ETS-2 (Kiku-2)	GTO	3rd stage used
15 February 1978, 04:00	4(F)	ISS-2 (JISS-2/Ume-2)	LEO
6 February 1979, 08:46	5(F)	ECS-A (Ayame-1)	GTO	3rd stage used Failure – Recontact between satellite and upper stage.
22 February 1980, 08:35	6(F)	ECS-B (Ayame-2)	GTO	3rd stage used
3 September 1982, 05:00	9(F)	ETS-3 (Kiku-3)	LEO

See also

• Comparison of orbital launchers families
• Delta rocket
• H-I
• H-II
• H-IIA
• PGM-17 Thor