LGM-30 Minuteman

LGM-30 Minuteman
(LGM-30 Pang-bô͘:絡 Pang-bô͘:絡)
LGM-30 Minuteman; (LGM-30 Pang-bô͘:絡 Pang-bô͘:絡)
	; Minuteman II
類型	Intercontinental ballistic missile
原產地	Bíkok
服役記錄
服役期間	1962-1969Pang-bô͘:Nbsp(Minuteman伊); 1965-1994Pang-bô͘:Nbsp(Minuteman II); 1970-bo̍ktsênPang-bô͘:Nbsp(Minuteman III);
使用者	Bíkok
生產歷史
生產商	Boeing
丹計	$7,000,000 USD
基本資源
重量	About 65,000 lb (29,000 kg) (Minuteman伊); About 73,000 lb (33,000 kg) (Minuteman II); 79,432 lb (36,030 kg) (Minuteman III);
腸肚	53 ft 8 in (16.36 m) (Minuteman I/A); 55 ft 11 in (17.04 m) (Minuteman I/B); 57 ft 7 in (17.55 m) (Minuteman II); 59.9 ft (18.3 m) (Minuteman III);
直徑	5 ft 6 in (1.68 m) (第1 tset)
Tuâñ頭	MMI: W59 (退役); MMI and MMII: W56 (退役); MMIII: W62 (退役)，W78 (服譯)，或者W87 (服譯)
Detonation; mechanism	空氣爆破或者接屬 (表面)
E̋n-z̩引	3 tset solid-fuel rocket e̋n-ⱬín; 第1 tset: Thiokol 蛛122 (M-55) (178,000 lbf， 792 kN); 第2 tset: Aerojet-General SR-19-AJ-1 (60,181 lbf， 267.7 kN); 第3 tset: Aerojet/Thiokol SR73-AJ/TC-1 (34,170 lbf， 152 kN); ; 第1 tset 202,600 lb (91,900 kg) (Minuteman III)
推進去	Ammonium perchlorate composite propellant
運作範圍	10,000 km (6,200 mi) (Minuteman III)
飛行星限	700 mi (3,700,000 ft; 1,100 km)
上權速度	Mach 23; (17,508 miles per hour; 28,176 kilometers per hour; 7.8267 kilometers per second) (做買tset)
道引系統	Inertial NS-50
精確率	MMI: 1.1 nmi (2.0 km) CEP相開始，然後 0.6 nmi (1.1 km) CEP; MMII: 0.26 nmi (0.48 km) CEP; MMIII: 800 ft (240 m) CEP
發射; pêñ台	Pang-bô͘:Ill

LGM-30 Minuteman (英語 (ing-gú): LGM-30 Minuteman; 漢語 (hàn-gú): LGM-30 Pang-bô͘:Ill Pang-bô͘:Ill) 是 (sī) Pang-bô͘:Ill服役 (ho̍k-i̍k)的 (ê)陸基 (lio̍k-ki) Pang-bô͘:Ill (ICBM)，就是 (tio̍h-sī)代表 (tāi-piáu)美國 (Bí-kok) Pang-bô͘:Ill的陸地 (lio̍k-tē)導彈 (tō-tān)基礎 (ki-tshóo)。浙指 (Tsiat-tsí)2021年 (nî)， LGM-30G Minuteman III行 (hîng)的版本 (pán-pún)^{[注 1]}是美國唯一 (uî-it)服譯 (ho̍k-i̍k)的陸基 Pang-bô͘:Ill，佮 (kah) Pang-bô͘:Ill Pang-bô͘:Ill (SLBM) 和 (hām)遠程 (uán-tîng) Pang-bô͘:Ill扎著 (tsah-tio̍h)核武器 (hi̍k-bú-khì)。

註釋 (Tsù-sik)[修改]

↑ The letter "L" in "LGM" indicates that the missile is Pang-bô͘:絡-launched; the "G" indicates that it is designed to attack ground targets; the "M" indicates that it is a guided missile.

註解 (Tsù-kái)[修改]

↑ "Minuteman I".
↑ "Minuteman II".
↑ "Minuteman III".
↑ ^4.0 ^4.1 ^4.2 ^4.3 ^4.4 ^4.5 ^4.6 "Minuteman III". csis.org (ēng Eng-gí). Center for Strategic and International Studies. 2018-06-15. 2021-03-26 khòaⁿ--ê.
↑ "LGM-30G Minuteman III > Air Force > Fact Sheet Display". Af.mil. 2017-07-31. 2022-08-15 khòaⁿ--ê.

參考 (Tsham-khó)文 (bûn)hèn[修改]

Heefner, Gretchen (2012-09-12). The Missile Next Door: The Minuteman in the American Heartland (ēng Eng-gí) (Sew pán.). Harvard University Press. ISBN 978-0674059115. LCCN 2012003666. OCLC 872141698. OL 25190410M.
Lloyd, Alwyn T。 (2000-01-15). Cold War Legacy: A Tribute都the Strategic Air Command: 1946–1992 (ēng Eng-gí) (1st pán.). Pictorial Histories Publishing Company. ISBN 978-1575100524. OCLC 44672618. OL 8744142M.
McMurran, Marshal William (2008-12-11). Achieving Accuracy: A Legacy of Computers and Missiles (ēng Eng-gí). Xlibris. ISBN 978-1436381079. OCLC 302388811. ^{[unreliable source?]}^{[self-published source]}
Neal, Roy (2011-05-09). Ace in the Hole: The Story of the Minuteman Missile (ēng Eng-gí). Doubleday 1962 chhhut-pán. ISBN 978-1258013622. OCLC 952016433.
ICBM Prime Team - TRW Systems (2001-07-01). "Minuteman Weapon System History and Description" (PDF). nukestrat.com (ēng Eng-gí). TRW Inc. goân-loē-iông (PDF) tī 2019-08-05 hőng khó͘-pih. 2019-11-22 khòaⁿ--ê – via Hans M。 Kristensen.
Neal, Roy (2011-05-09). Ace in the Hole: The Story of the Minuteman Missile (ēng Eng-gí). Doubleday 1962 chhhut-pán. ISBN 978-1258013622. OCLC 952016433.
Zuckerman, Edward (1984-06-04). The Day After World War III (ēng Eng-gí). Viking Press. ISBN 978-0670258802. LCCN 83040230. OCLC 869504401. OL 3184958M. 2019-11-22 khòaⁿ--ê – via Internet Archive.

Ên身 (sin)娃 (ua)̽t-to̽k[修改]

The Boeing Corporation (1973). Technical Order 21M-LGM30G-1-1: Minuteman Weapon System Description. (英語)
The Boeing Corporation (1973). Technical Order 21M-LGM30G-1-22: Minuteman Weapon System Operations. (英語)
The Boeing Corporation (1994). Technical Order 21M-LGM30G-2-1-7: Organizational Maintenance Control， Minuteman Weapon System. (英語)

參閱 (Tsham-ua̍t)[修改]

外部 (Guā-pōo)lên-ket[修改]

佇Wikimedia Commons等的相關檔案: Minuteman

[6] The letter "L" in "LGM" indicates that the missile is Pang-bô͘:絡-launched; the "G" indicates that it is designed to attack ground targets; the "M" indicates that it is a guided missile.

[1] "Minuteman I".

[2] "Minuteman II".

[3] "Minuteman III".

[FAS_LGM-30-3-4] 4.0 ^4.1 ^4.2 ^4.3 ^4.4 ^4.5 ^4.6 "Minuteman III". csis.org (ēng Eng-gí). Center for Strategic and International Studies. 2018-06-15. 2021-03-26 khòaⁿ--ê.

[5] "LGM-30G Minuteman III > Air Force > Fact Sheet Display". Af.mil. 2017-07-31. 2022-08-15 khòaⁿ--ê.

[1]

[2]

[3]

[4]

[5]

[注 1]

LGM-30 Minuteman

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註釋 (Tsù-sik)[修改]

註解 (Tsù-kái)[修改]

參考 (Tsham-khó)文 (bûn)hèn[修改]

Ên身 (sin)娃 (ua)̽t-to̽k[修改]

參閱 (Tsham-ua̍t)[修改]

外部 (Guā-pōo)lên-ket[修改]

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LGM-30 Minuteman (LGM-30 Pang-bô͘:絡 Pang-bô͘:絡)
Minuteman II
類型	Intercontinental ballistic missile
原產地	Bíkok
服役記錄
服役期間	1962-1969^[1]Pang-bô͘:Nbsp(Minuteman伊) 1965-1994^[2]Pang-bô͘:Nbsp(Minuteman II) 1970-bo̍ktsên^[3]Pang-bô͘:Nbsp(Minuteman III)
使用者	Bíkok
生產歷史
生產商	Boeing^[4]
丹計	$7,000,000 USD^[4]
基本資源
重量	About 65,000 lb (29,000 kg) (Minuteman伊) About 73,000 lb (33,000 kg) (Minuteman II) 79,432 lb (36,030 kg) (Minuteman III)^[4]
腸肚	53 ft 8 in (16.36 m) (Minuteman I/A) 55 ft 11 in (17.04 m) (Minuteman I/B) 57 ft 7 in (17.55 m) (Minuteman II) 59.9 ft (18.3 m) (Minuteman III)^[4]
直徑	5 ft 6 in (1.68 m) (第1 tset)
Tuâñ頭	MMI: W59 (退役) MMI and MMII: W56 (退役) MMIII: W62 (退役)，W78 (服譯)，或者W87 (服譯)
Detonation mechanism	空氣爆破或者接屬 (表面)

E̋n-z̩引	3 tset solid-fuel rocket e̋n-ⱬín 第1 tset: Thiokol 蛛122 (M-55) (178,000 lbf， 792 kN) 第2 tset: Aerojet-General SR-19-AJ-1 (60,181 lbf， 267.7 kN) 第3 tset: Aerojet/Thiokol SR73-AJ/TC-1 (34,170 lbf， 152 kN) 第1 tset 202,600 lb (91,900 kg) (Minuteman III)^[4]
推進去	Ammonium perchlorate composite propellant
運作範圍	10,000 km (6,200 mi) (Minuteman III)^[5]
飛行星限	700 mi (3,700,000 ft; 1,100 km)^[4]
上權速度	Mach 23 (17,508 miles per hour; 28,176 kilometers per hour; 7.8267 kilometers per second) (做買tset)^[4]
道引系統	Inertial NS-50
精確率	MMI: 1.1 nmi (2.0 km) CEP相開始，然後 0.6 nmi (1.1 km) CEP MMII: 0.26 nmi (0.48 km) CEP MMIII: 800 ft (240 m) CEP
發射 pêñ台	Pang-bô͘:Ill