N-I_(rocket) Knowpia

Summary

N-I
Size
The N-I rocket^[1]
Function	Carrier rocket
Manufacturer	McDonnell Douglas (design) Mitsubishi Heavy Industries (production)
Country of origin	United States (design) Japan (production)
Height	34 metres (112 ft)^[1]
Diameter	2.44 metres (8.0 ft)
Mass	131,330 kilograms (289,530 lb)^[1]
Stages	2 or 3
Capacity
Payload to LEO
Mass	1,200 kilograms (2,600 lb)^[1]
Payload to GTO
Mass	360 kilograms (790 lb)^[1]

Associated rockets
Family	Delta
Launch history
Status	Retired
Launch sites	LA-N, Tanegashima
Total launches	7
Success(es)	6
Partial failure(s)	1
First flight	9 September 1975
Last flight	3 September 1982

Boosters – Castor 2
No. boosters	3^[2]
Engines	1 TX-354-3
Thrust	258.9 kilonewtons (58,200 lbf)
Specific impulse	262 sec
Burn time	37 seconds
Fuel	Solid
First stage – Thor-ELT
Engines	1 MB-3-3
Thrust	866.7 kilonewtons (194,800 lbf)
Specific impulse	290 sec
Burn time	270 seconds
Fuel	RP-1/LOX
Second stage
Engines	1 LE-3
Thrust	52.9 kilonewtons (11,900 lbf)
Specific impulse	290 sec
Burn time	246 seconds
Fuel	NTO/A-50
Third stage (optional) – Star-37N
Engines	1 solid
Thrust	45 kilonewtons (10,000 lbf)
Specific impulse	290 sec
Burn time	42 seconds
Fuel	Solid

Mock up of N-1

The N-I or N-1 was a derivative of the American Thor-Delta rocket, produced under license in Japan. The N stood for "Nippon" (Japan). It used a Long Tank Thor first stage, a Mitsubishi Heavy Industries-designed LE-3 engine on the second stage,^[3]^[4]^[5] and three Castor SRMs.^[2]^[6] 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.^[7]

Launch history

Flight No.	Date / time (UTC)	Launch site	Payload	Orbit	Launch outcome
1(F)	9 September 1975 05:30^[8]	Tanegashima	ETS-1 (JETS-1/Kiku-1)^[9]	LEO	Success
1(F)
2(F)	29 February 1976 03:30^[8]	Tanegashima	ISS-1 (JISS-1/Ume-1)^[10]	LEO	Success
2(F)
3(F)	23 February 1977 08:50^[8]	Tanegashima	ETS-2 (Kiku-2)^[11]	GTO	Success
3(F)	3rd stage used
4(F)	16 February 1978 04:00^[8]	Tanegashima	ISS-2 (JISS-2/Ume-2)^[10]	LEO	Success
4(F)
5(F)	6 February 1979 08:46^[8]	Tanegashima	ECS-A (Ayame-1)^[12]	GTO	Partial failure
5(F)	3rd stage used; Recontact between satellite and upper stage.
6(F)	22 February 1980 08:35^[8]	Tanegashima	ECS-B (Ayame-2)^[12]	GTO	Success
6(F)	3rd stage used
9(F)	3 September 1982 05:00^[8]	Tanegashima	ETS-3 (Kiku-4)^[13]	LEO	Success
9(F)

References

^ ^a ^b ^c ^d ^e Wade, Mark. "Delta". Encyclopedia Astronautica. Archived from the original on 22 May 2013. Retrieved 3 September 2008.
^ ^a ^b "JAXA Digital Archives". Japan Aerospace Exploration Agency. Archived from the original on 9 September 2009. Retrieved 1 October 2009.
^ "N-Iロケット開発の歩み". Yukihiko Takenaka, NASDA. Retrieved 10 February 2011.^{[permanent dead link]}
^ "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.
^ "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.
^ Krebs, Gunter. "N-1". Gunter's Space Page. Retrieved 31 August 2008.
^ Pearlman, Robert. "Space Station Command Change Is One Giant Leap (Day) for Space History". Space.com. Retrieved 2 November 2017.
^ ^a ^b ^c ^d ^e ^f ^g McDowell, Jonathan. "Thor". Orbital and Suborbital Launch Database. Jonathan's Space Report. Retrieved 31 August 2008.
^ "JAXA | Engineering Test Satellite I "KIKU-1" (ETS-I)". JAXA | Japan Aerospace Exploration Agency. Retrieved 16 March 2020.
^ ^a ^b "JAXA | Ionosphere Sounding Satellite "UME" (ISS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 16 March 2020.
^ "JAXA | Engineering Test Satellite II "KIKU-2" (ETS-II)". JAXA | Japan Aerospace Exploration Agency. Retrieved 16 March 2020.
^ ^a ^b "JAXA | Experimental Communications Satellites "Ayame" (ECS)". JAXA | Japan Aerospace Exploration Agency. Retrieved 16 March 2020.
^ "JAXA | Engineering Test Satellite III "KIKU-4" (ETS-III)". JAXA | Japan Aerospace Exploration Agency. Retrieved 16 March 2020.

Mitsubishi Heavy Industries

Mitsubishi

Subsidiaries

Joint ventures

Current	Atmea Japanese Aero Engine Corporation Launch Services Alliance
Defunct	Nihon Aircraft Manufacturing Corporation

Products

Aircraft	F-1 F-2 F-15J H-60 MH2000 Mitsubishi SpaceJet T-2 X-2
Armored vehicles	Type 10 Type 61 Type 74 Nana-yon Type 89 IFV Type 90 Kyū-maru
Launch vehicles	N-I N-II H-I H-II H-IIA H-IIB H3
Missiles	Type 88 Type 89 Type 90 Type 91
Ships	Akizuki class Atago class Hatakaze class Kongō class Takanami class
Submarines	Harushio class Oyashio class Sōryū class
Other	Crystal Mover Green Mover Max MEISTeR Mitsubishi APWR Wakamaru

People

Kazuo Tsukuda

Other

Mitsubishi Sagamihara DynaBoars

Products currently in development shown in italics

Category

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara A5 Antares 230+ Ariane 5 Atlas V Ceres-1 Delta IV Heavy Electron Epsilon Falcon 9 Block 5 Falcon Heavy GSLV Mk II Mk III H-IIA Hyperbola-1 Jielong 1 Kuaizhou 1 1A 11^† Kaituozhe 2 LauncherOne Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 7 7A 8 11 Minotaur I IV V C OS-M1^† Pegasus XL Proton-M PSLV Qased Rocket 3^† Safir Shavit Simorgh^† Soyuz-2 2.1a / STA 2.1b / STB 2-1v Unha Vega Zenit 3SL 3SLB 3F Zhuque-1^†
In development	Agnibaan Amur Angara 1.2 Antariksh - 1 Ariane 6 Bloostar Chetak Cyclone-4M Eris Firefly Alpha Beta H3 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 921 rocket 9 Miura 5 Neutron New Glenn New Line 1 Nuri OS-M2 OS-M4 Orbex Prime Phoenix SLV-1T SLV-VT SLS Soyuz-7 SSLV Starship Terran 1 Terran R Vega C Vega E Vikram - I Vikram - II Vikram - III Vulcan Zero Zhuque-2
Retired	Antares 110 120 130^† 230 Ariane 1 2 3 4 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV Diamant Dnepr Energia Europa^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos 1 2I 3 3M Lambda 4S Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Saturn I IB V Scout SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard VLS-1^† Zenit 2 2M
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates historical or current rockets that attempted orbital launches but did not ever succeed (never did or has performed a successful orbital launch)

Japanese orbital launch systems

JAXA

Active	Epsilon H-IIA SS-520(Three stage variant)
Planned	H3
Retired	H-IIB

ISAS

Retired	Lambda (4S) Mu (4S 3C 3H 3S 3SII V)

NASDA

Retired	N-I‡ N-II‡ H-I‡ H-II

Other

Planned	ZERO
Cancelled	GX‡
Development halted	J-I¤

‡ Based around licence-produced US rockets; ¤ Never flew an orbital flight (only 1 suborbital flight performed)

Thor and Delta rockets

Rockets

Thor

Delta

Alphabetical	Delta A Delta B Delta C Delta D Delta E Delta F Delta G Delta J Delta L Delta M Delta N
Numerical	Delta 0100 Delta 1000 Delta 2000 Delta 3000 Delta 4000 Delta 5000 Delta 6000 Delta 7000 Delta 8000 Delta 9000
Modern	Delta II Delta III Delta IV Delta IV Heavy

Export

Launch sites

Canaveral	(S)LC-17 LC-18B SLC-37B
Johnston	LE-1 LE-2
Tanegashima	Osaki
Vandenberg	SLC-1 SLC-2 SLC-3 SLC-6 SLC-10
Bases	Bardney Breighton Caistor Carnaby Catfoss Coleby Grange Driffield Feltwell Folkingham Full Sutton Harrington Hemswell Ludford Magna Melton Mowbray Mepal North Luffenham North Pickenham Polebrook Shepherds Grove Tuddenham

Components

Boosters

First stages

Common Booster Core

Upper Stages

Delta	Delta-A Delta-D Delta-E Delta-F Delta-K Delta-P DCSS
Other	Able Ablestar Agena Altair Burner FW-4D IABS PAM-D Star UM-129

Engines

Manufacturers

Rocket	Douglas McDonnell Douglas Boeing United Launch Alliance
Engines	Aerojet Alliant Rocketdyne Thiokol TRW

Launches

Summary

Launch history

See also

References