N-I (rocket)#Ionosphere Sounding Satellite "UME-2" (ISS-b)
{{Short description|Booster}}
{{about|the Japanese rocket|the Soviet rocket|N1 (rocket)}}
{{Use dmy dates|date=October 2020}}
{{Infobox Rocket
|name = N-I
|image=N-I.svg
|caption = The N-I rocket{{cite web|url=http://www.astronautix.com/lvs/delta.htm|title=Delta|first=Mark|last=Wade|publisher=Encyclopedia Astronautica|access-date=3 September 2008|url-status=dead|archive-url=https://web.archive.org/web/20130817180906/http://astronautix.com/lvs/delta.htm|archive-date=17 August 2013|df=dmy-all}}
|function = Carrier rocket
|manufacturer = McDonnell Douglas (design)
Mitsubishi Heavy Industries (production)
|country-origin = United States (design)
Japan (production)
|diameter = {{convert|2.44|m|ft}}
|mass = {{convert|131330|kg|lb}}
|stages = 2 or 3
|capacities =
{{Infobox Rocket/Payload
|location = LEO
|kilos = {{convert|1200|kg|lb}}
}}
{{Infobox Rocket/Payload
|location = GTO
|kilos = {{convert|360|kg|lb}}
}}
|family = Delta
|status = Retired
|sites = Tanegashima, Osaki
|launches = 7
|success = 6
|partial = 1
|first = 9 September 1975
|last = 3 September 1982
|stagedata =
{{Infobox Rocket/Stage
|type = booster
|name = Castor 2
|engines = 1 TX-354-3
|thrust = {{convert|258.9|kN|lbf}}
|SI = 262 sec
|burntime = 37 seconds
|fuel = Solid
}}
{{Infobox Rocket/Stage
|type = stage
|stageno = First
|name = Thor-ELT
|engines = 1 MB-3-3
|thrust = {{convert|866.7|kN|lbf}}
|SI = 290 sec
|burntime = 270 seconds
}}
{{Infobox Rocket/Stage
|type = stage
|name =
|stageno = Second
|engines = 1 LE-3
|thrust = {{convert|52.9|kN|lbf}}
|SI = 290 sec
|burntime = 246 seconds
}}
{{Infobox Rocket/Stage
|type = stage
|name = Star-37N
|stageno = Third
|diff = optional
|engines = 1 solid
|thrust = {{convert|45|kN|lbf}}
|SI = 290 sec
|burntime = 42 seconds
|fuel = Solid
}}
}}
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,{{cite web|url=https://www.jstage.jst.go.jp/article/jjsass1969/32/362/32_362_127/_pdf/-char/ja|title=N-Iロケット開発の歩み|publisher=Yukihiko Takenaka, NASDA|access-date=10 February 2011}}{{cite web|url=http://202.228.55.2/ngpsw/introduction/history/index.html|title=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|publisher=Mitsubishi Heavy Industries|access-date=10 February 2011|url-status=dead|archive-url=https://web.archive.org/web/20110704102309/http://202.228.55.2/ngpsw/introduction/history/index.html|archive-date=4 July 2011}}{{cite web|url=http://www.mext.go.jp/b_menu/hakusho/html/hpaa198201/hpaa198201_2_030.html|title=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|publisher=Ministry of Education, Culture, Sports, Science and Technology|access-date=10 February 2011|archive-url=https://web.archive.org/web/20080615025750/http://www.mext.go.jp/b_menu/hakusho/html/hpaa198201/hpaa198201_2_030.html|archive-date=15 June 2008|url-status=dead}} and three Castor SRMs.{{cite web|url=http://jda.jaxa.jp/jda/p1_e.php|title=JAXA Digital Archives|publisher=Japan Aerospace Exploration Agency|access-date=1 October 2009|url-status=dead|archive-url=https://web.archive.org/web/20090909144812/http://jda.jaxa.jp/jda/p1_e.php|archive-date=9 September 2009}}{{cite web|url=http://space.skyrocket.de/doc_lau_det/n-1.htm|title=N-1|first=Gunter|last=Krebs|publisher=Gunter's Space Page|access-date=31 August 2008}} 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, as of 17 February 2024, to occur on a leap day.{{cite web|url=https://www.space.com/32093-space-station-leap-day-spaceflight-history.html|title=Space Station Command Change Is One Giant Leap (Day) for Space History|first=Robert|last=Pearlman|date=29 February 2016 |publisher=Space.com|access-date=2 November 2017}}
Launch history
class="wikitable plainrowheaders" |
scope="col" | Flight No.
! scope="col" | Date / time (UTC) ! scope="col" | Launch site ! scope="col" | Payload{{Cite web |title=JAXA {{!}} N-I Launch Vehicle |url=https://global.jaxa.jp/projects/rockets/n1/ |access-date=2024-02-18 |website=JAXA {{!}} Japan Aerospace Exploration Agency |language=en}} ! scope="col" | Payload mass ! scope="col" | Orbit ! scope="col" | Launch |
---|
scope="row" rowspan = 2 style="text-align:center;|1(F)
| 9 September 1975 | Engineering Test Satellite I "KIKU-1"(ETS-I) | LEO | {{Success}} |
colspan="6" | |
scope="row" rowspan = 2 style="text-align:center;|2(F)
| Ionosphere Sounding Satellite "UME"(ISS) | LEO | {{Success}} |
colspan="6" | |
scope="row" rowspan = 2 style="text-align:center;|3(F)
| Engineering Test Satellite II "KIKU-2"(ETS-II) | GTO | {{Success}} |
colspan="6" |3rd stage used |
scope="row" rowspan = 2 style="text-align:center;|4(F)
| Ionosphere Sounding Satellite "UME-2"(ISS-b) | LEO | {{Success}} |
colspan="6" | |
scope="row" rowspan = 2 style="text-align:center;|5(F)
| Experimental Communications Satellites "Ayame"(ECS) | GTO | {{Partial failure}} |
colspan="6" |3rd stage used; Recontact between satellite and upper stage. |
scope="row" rowspan = 2 style="text-align:center;|6(F)
| Experimental Communications Satellites "Ayame-2"(ECS-b) | GTO | {{Success}} |
colspan="6" |3rd stage used; Satellite failed shortly after separation. |
scope="row" rowspan = 2 style="text-align:center;|9(F)
| Engineering Test Satellite III "KIKU-4"(ETS-III) | LEO | {{Success}} |
colspan="6" | |
Payload Descriptions
= Engineering Test Satellite I "KIKU-1" (ETS-1) =
ETS-1 was the first satellite launched by the NASDA. It had the objective of acquiring information on N-series launch vehicles, orbit injection, and tracking and control. It ceased operations on 28 April 1982.
= Ionosphere Sounding Satellite "UME" (ISS) =
UME was Japan's first Ionosphere Sounding Satellite. It was used to monitor radio waves in the ionosphere and forecast conditions for shortwave communications. A power supply issue caused Ume to stop functioning one month after launch.{{Cite web |title=ISS a, b (Ume 1, 2) |url=https://space.skyrocket.de/doc_sdat/iss-a.htm |access-date=2024-02-18 |website=Gunter's Space Page |language=en}}
= Engineering Test Satellite II "KIKU-2" (ETS-2) =
KIKU-2 was NASDA's first satellite launched to GEO. It was intended to gather data on geostationary satellite launch, tracking, control, orbit maintenance, and attitude control as well as carrying out experiments on communications equipment. KIKU-2 ceased operations on 10 December 1990, leaving GEO.
= Ionosphere Sounding Satellite "UME-2" (ISS-b) =
UME-2 had similar goals to the original UME satellite, but was much more successful in carrying them out. While it was originally intended to gather data for only a year and a half, UME-2 ceased operations on 23 February 1983.
= Experimental Communications Satellites "Ayame/Ayame-2" (ECS/ECS-b) =
Both ECS satellites were unsuccessful in completing their mission. During the first ECS launch, the third stage rocket collided with the satellite shortly after separation. During the ECS-2 launch, the satellite stopped transmitting shortly after separation. The satellites had the intention of conducting millimeter wave experiments. The JAXA website states that "we learned some valuable lessons on satellite separation technology and apogee engine from this experience".
= About Engineering Test Satellite III "KIKU-4" (ETS-III) =
KIKU-4 was developed to acquire data on designing earth observation satellites with high power requirements. KIKU-4 completed testing of three-axis attitude control, deployable solar panels, movable heat control, and ion engine operation. On 8 April 1985, the satellite ran out of fuel and ceased operation.
See also
References
{{reflist|colwidth=30em}}
{{Mitsubishi Heavy Industries}}
{{Expendable launch systems}}
{{Japanese launch systems}}
{{Thor and Delta rockets}}
Category:Mitsubishi Heavy Industries space launch vehicles