How much propellant is used up until liftoff?Challenger disaster: how full was the external tank at the time of destruction?How does the Space Shuttle's SSME engine's thrust vary after ignition?What rocket uses the largest percentage of Fuel/Oxidizer before liftoff?How much fuel was used for a Space Shuttle launch?SpaceX Falcon 9 Reusable first stage propellant for returnPropellant mass calculationHow does the mass of launchers change over time between ground and orbit?chemical propulsion with separate fuel and propellant?Is HAN-water propellant “green” enough to ever be used in a cubesat?What was the result of the propellant predictions in the last chapter of “Ignition!”?How to transport gigawatt-level power across a 100km distance?How to determine $Delta v$ loss due to gravitational pull from earthHow much fuel is necessary for 2nd stage of Falcon 9 rocket to land?

Hackerrank All Women's Codesprint 2019: Name the Product

Asserting that Atheism and Theism are both faith based positions

Have the tides ever turned twice on any open problem?

Print a physical multiplication table

Unfrosted light bulb

Determine voltage drop over 10G resistors with cheap multimeter

Why do I have a large white artefact on the rendered image?

Do native speakers use "ultima" and "proxima" frequently in spoken English?

PTIJ: At the Passover Seder, is one allowed to speak more than once during Maggid?

Fair way to split coins

Help with identifying unique aircraft over NE Pennsylvania

What is the tangent at a sharp point on a curve?

Knife as defense against stray dogs

Air travel with refrigerated insulin

Should a narrator ever describe things based on a characters view instead of fact?

What is the reasoning behind standardization (dividing by standard deviation)?

Was World War I a war of liberals against authoritarians?

How can a new country break out from a developed country without war?

Pre-Employment Background Check With Consent For Future Checks

Homology of the fiber

What is 管理しきれず?

Jem'Hadar, something strange about their life expectancy

How can an organ that provides biological immortality be unable to regenerate?

How to balance a monster modification (zombie)?



How much propellant is used up until liftoff?


Challenger disaster: how full was the external tank at the time of destruction?How does the Space Shuttle's SSME engine's thrust vary after ignition?What rocket uses the largest percentage of Fuel/Oxidizer before liftoff?How much fuel was used for a Space Shuttle launch?SpaceX Falcon 9 Reusable first stage propellant for returnPropellant mass calculationHow does the mass of launchers change over time between ground and orbit?chemical propulsion with separate fuel and propellant?Is HAN-water propellant “green” enough to ever be used in a cubesat?What was the result of the propellant predictions in the last chapter of “Ignition!”?How to transport gigawatt-level power across a 100km distance?How to determine $Delta v$ loss due to gravitational pull from earthHow much fuel is necessary for 2nd stage of Falcon 9 rocket to land?













8












$begingroup$


How much of the total propellant mass (fuel+oxidizer) of the first stage/boosters is usually burnt between ignition and liftoff?










share|improve this question









$endgroup$











  • $begingroup$
    two percent plus or minus one percent
    $endgroup$
    – uhoh
    16 hours ago










  • $begingroup$
    @uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
    $endgroup$
    – Organic Marble
    14 hours ago










  • $begingroup$
    @OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
    $endgroup$
    – uhoh
    14 hours ago











  • $begingroup$
    My wheelhouse is pretty narrow.
    $endgroup$
    – Organic Marble
    14 hours ago















8












$begingroup$


How much of the total propellant mass (fuel+oxidizer) of the first stage/boosters is usually burnt between ignition and liftoff?










share|improve this question









$endgroup$











  • $begingroup$
    two percent plus or minus one percent
    $endgroup$
    – uhoh
    16 hours ago










  • $begingroup$
    @uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
    $endgroup$
    – Organic Marble
    14 hours ago










  • $begingroup$
    @OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
    $endgroup$
    – uhoh
    14 hours ago











  • $begingroup$
    My wheelhouse is pretty narrow.
    $endgroup$
    – Organic Marble
    14 hours ago













8












8








8





$begingroup$


How much of the total propellant mass (fuel+oxidizer) of the first stage/boosters is usually burnt between ignition and liftoff?










share|improve this question









$endgroup$




How much of the total propellant mass (fuel+oxidizer) of the first stage/boosters is usually burnt between ignition and liftoff?







launch fuel efficiency






share|improve this question













share|improve this question











share|improve this question




share|improve this question










asked 17 hours ago









Everyday AstronautEveryday Astronaut

2,096832




2,096832











  • $begingroup$
    two percent plus or minus one percent
    $endgroup$
    – uhoh
    16 hours ago










  • $begingroup$
    @uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
    $endgroup$
    – Organic Marble
    14 hours ago










  • $begingroup$
    @OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
    $endgroup$
    – uhoh
    14 hours ago











  • $begingroup$
    My wheelhouse is pretty narrow.
    $endgroup$
    – Organic Marble
    14 hours ago
















  • $begingroup$
    two percent plus or minus one percent
    $endgroup$
    – uhoh
    16 hours ago










  • $begingroup$
    @uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
    $endgroup$
    – Organic Marble
    14 hours ago










  • $begingroup$
    @OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
    $endgroup$
    – uhoh
    14 hours ago











  • $begingroup$
    My wheelhouse is pretty narrow.
    $endgroup$
    – Organic Marble
    14 hours ago















$begingroup$
two percent plus or minus one percent
$endgroup$
– uhoh
16 hours ago




$begingroup$
two percent plus or minus one percent
$endgroup$
– uhoh
16 hours ago












$begingroup$
@uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
$endgroup$
– Organic Marble
14 hours ago




$begingroup$
@uhoh if my system used 3% of its prop sitting on the pad, I would be unhappy.
$endgroup$
– Organic Marble
14 hours ago












$begingroup$
@OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
$endgroup$
– uhoh
14 hours ago





$begingroup$
@OrganicMarble we wouldn't want that. Are there any systems outside of my range? update: Oh, indeed there are!
$endgroup$
– uhoh
14 hours ago













$begingroup$
My wheelhouse is pretty narrow.
$endgroup$
– Organic Marble
14 hours ago




$begingroup$
My wheelhouse is pretty narrow.
$endgroup$
– Organic Marble
14 hours ago










1 Answer
1






active

oldest

votes


















11












$begingroup$

For the Space Shuttle:



Using the same approximate curves (with all their assumptions and limitations) used in the answer to How does the Space Shuttle's SSME engine's thrust vary after ignition?, we can integrate the SSME flowrates to get a startup propellant consumption of:



416 lbm LH2, 2246 lbm LO2 per engine,



and ~ 1248 lbm LH2, 6738 lbm LO2 for all three engines.



Since liftoff was virtually instantaneous after SRB ignition (certainly to the precision of these calculations) we can ignore SRB propellant usage preliftoff.



Using the ET loading numbers from Challenger disaster: how full was the external tank at the time of destruction? (LO2 1,387,457 lbm, LH2 234,265 lbm) we can calculate the % usage of ET propellant prior to liftoff as approximately 0.5% for both propellants.






share|improve this answer











$endgroup$












  • $begingroup$
    The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
    $endgroup$
    – Uwe
    15 hours ago










  • $begingroup$
    @Uwe I was actually editing that into my answer as you were posting....
    $endgroup$
    – Organic Marble
    15 hours ago










Your Answer





StackExchange.ifUsing("editor", function ()
return StackExchange.using("mathjaxEditing", function ()
StackExchange.MarkdownEditor.creationCallbacks.add(function (editor, postfix)
StackExchange.mathjaxEditing.prepareWmdForMathJax(editor, postfix, [["$", "$"], ["\\(","\\)"]]);
);
);
, "mathjax-editing");

StackExchange.ready(function()
var channelOptions =
tags: "".split(" "),
id: "508"
;
initTagRenderer("".split(" "), "".split(" "), channelOptions);

StackExchange.using("externalEditor", function()
// Have to fire editor after snippets, if snippets enabled
if (StackExchange.settings.snippets.snippetsEnabled)
StackExchange.using("snippets", function()
createEditor();
);

else
createEditor();

);

function createEditor()
StackExchange.prepareEditor(
heartbeatType: 'answer',
autoActivateHeartbeat: false,
convertImagesToLinks: false,
noModals: true,
showLowRepImageUploadWarning: true,
reputationToPostImages: null,
bindNavPrevention: true,
postfix: "",
imageUploader:
brandingHtml: "Powered by u003ca class="icon-imgur-white" href="https://imgur.com/"u003eu003c/au003e",
contentPolicyHtml: "User contributions licensed under u003ca href="https://creativecommons.org/licenses/by-sa/3.0/"u003ecc by-sa 3.0 with attribution requiredu003c/au003e u003ca href="https://stackoverflow.com/legal/content-policy"u003e(content policy)u003c/au003e",
allowUrls: true
,
noCode: true, onDemand: true,
discardSelector: ".discard-answer"
,immediatelyShowMarkdownHelp:true
);



);













draft saved

draft discarded


















StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f34893%2fhow-much-propellant-is-used-up-until-liftoff%23new-answer', 'question_page');

);

Post as a guest















Required, but never shown

























1 Answer
1






active

oldest

votes








1 Answer
1






active

oldest

votes









active

oldest

votes






active

oldest

votes









11












$begingroup$

For the Space Shuttle:



Using the same approximate curves (with all their assumptions and limitations) used in the answer to How does the Space Shuttle's SSME engine's thrust vary after ignition?, we can integrate the SSME flowrates to get a startup propellant consumption of:



416 lbm LH2, 2246 lbm LO2 per engine,



and ~ 1248 lbm LH2, 6738 lbm LO2 for all three engines.



Since liftoff was virtually instantaneous after SRB ignition (certainly to the precision of these calculations) we can ignore SRB propellant usage preliftoff.



Using the ET loading numbers from Challenger disaster: how full was the external tank at the time of destruction? (LO2 1,387,457 lbm, LH2 234,265 lbm) we can calculate the % usage of ET propellant prior to liftoff as approximately 0.5% for both propellants.






share|improve this answer











$endgroup$












  • $begingroup$
    The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
    $endgroup$
    – Uwe
    15 hours ago










  • $begingroup$
    @Uwe I was actually editing that into my answer as you were posting....
    $endgroup$
    – Organic Marble
    15 hours ago















11












$begingroup$

For the Space Shuttle:



Using the same approximate curves (with all their assumptions and limitations) used in the answer to How does the Space Shuttle's SSME engine's thrust vary after ignition?, we can integrate the SSME flowrates to get a startup propellant consumption of:



416 lbm LH2, 2246 lbm LO2 per engine,



and ~ 1248 lbm LH2, 6738 lbm LO2 for all three engines.



Since liftoff was virtually instantaneous after SRB ignition (certainly to the precision of these calculations) we can ignore SRB propellant usage preliftoff.



Using the ET loading numbers from Challenger disaster: how full was the external tank at the time of destruction? (LO2 1,387,457 lbm, LH2 234,265 lbm) we can calculate the % usage of ET propellant prior to liftoff as approximately 0.5% for both propellants.






share|improve this answer











$endgroup$












  • $begingroup$
    The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
    $endgroup$
    – Uwe
    15 hours ago










  • $begingroup$
    @Uwe I was actually editing that into my answer as you were posting....
    $endgroup$
    – Organic Marble
    15 hours ago













11












11








11





$begingroup$

For the Space Shuttle:



Using the same approximate curves (with all their assumptions and limitations) used in the answer to How does the Space Shuttle's SSME engine's thrust vary after ignition?, we can integrate the SSME flowrates to get a startup propellant consumption of:



416 lbm LH2, 2246 lbm LO2 per engine,



and ~ 1248 lbm LH2, 6738 lbm LO2 for all three engines.



Since liftoff was virtually instantaneous after SRB ignition (certainly to the precision of these calculations) we can ignore SRB propellant usage preliftoff.



Using the ET loading numbers from Challenger disaster: how full was the external tank at the time of destruction? (LO2 1,387,457 lbm, LH2 234,265 lbm) we can calculate the % usage of ET propellant prior to liftoff as approximately 0.5% for both propellants.






share|improve this answer











$endgroup$



For the Space Shuttle:



Using the same approximate curves (with all their assumptions and limitations) used in the answer to How does the Space Shuttle's SSME engine's thrust vary after ignition?, we can integrate the SSME flowrates to get a startup propellant consumption of:



416 lbm LH2, 2246 lbm LO2 per engine,



and ~ 1248 lbm LH2, 6738 lbm LO2 for all three engines.



Since liftoff was virtually instantaneous after SRB ignition (certainly to the precision of these calculations) we can ignore SRB propellant usage preliftoff.



Using the ET loading numbers from Challenger disaster: how full was the external tank at the time of destruction? (LO2 1,387,457 lbm, LH2 234,265 lbm) we can calculate the % usage of ET propellant prior to liftoff as approximately 0.5% for both propellants.







share|improve this answer














share|improve this answer



share|improve this answer








edited 15 hours ago

























answered 15 hours ago









Organic MarbleOrganic Marble

58.9k3161252




58.9k3161252











  • $begingroup$
    The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
    $endgroup$
    – Uwe
    15 hours ago










  • $begingroup$
    @Uwe I was actually editing that into my answer as you were posting....
    $endgroup$
    – Organic Marble
    15 hours ago
















  • $begingroup$
    The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
    $endgroup$
    – Uwe
    15 hours ago










  • $begingroup$
    @Uwe I was actually editing that into my answer as you were posting....
    $endgroup$
    – Organic Marble
    15 hours ago















$begingroup$
The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
$endgroup$
– Uwe
15 hours ago




$begingroup$
The external tank is loaded with 1,387,457 lb of LOX and 234,265 lb of LH2. So only 0.5 % of LOX and also of LH2 are used before liftoff.
$endgroup$
– Uwe
15 hours ago












$begingroup$
@Uwe I was actually editing that into my answer as you were posting....
$endgroup$
– Organic Marble
15 hours ago




$begingroup$
@Uwe I was actually editing that into my answer as you were posting....
$endgroup$
– Organic Marble
15 hours ago

















draft saved

draft discarded
















































Thanks for contributing an answer to Space Exploration Stack Exchange!


  • Please be sure to answer the question. Provide details and share your research!

But avoid


  • Asking for help, clarification, or responding to other answers.

  • Making statements based on opinion; back them up with references or personal experience.

Use MathJax to format equations. MathJax reference.


To learn more, see our tips on writing great answers.




draft saved


draft discarded














StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f34893%2fhow-much-propellant-is-used-up-until-liftoff%23new-answer', 'question_page');

);

Post as a guest















Required, but never shown





















































Required, but never shown














Required, but never shown












Required, but never shown







Required, but never shown

































Required, but never shown














Required, but never shown












Required, but never shown







Required, but never shown







Popular posts from this blog

getting Checkpoint VPN SSL Network Extender working in the command lineHow to connect to CheckPoint VPN on Ubuntu 18.04LTS?Will the Linux ( red-hat ) Open VPNC Client connect to checkpoint or nortel VPN gateways?VPN client for linux machine + support checkpoint gatewayVPN SSL Network Extender in FirefoxLinux Checkpoint SNX tool configuration issuesCheck Point - Connect under Linux - snx + OTPSNX VPN Ububuntu 18.XXUsing Checkpoint VPN SSL Network Extender CLI with certificateVPN with network manager (nm-applet) is not workingWill the Linux ( red-hat ) Open VPNC Client connect to checkpoint or nortel VPN gateways?VPN client for linux machine + support checkpoint gatewayImport VPN config files to NetworkManager from command lineTrouble connecting to VPN using network-manager, while command line worksStart a VPN connection with PPTP protocol on command linestarting a docker service daemon breaks the vpn networkCan't connect to vpn with Network-managerVPN SSL Network Extender in FirefoxUsing Checkpoint VPN SSL Network Extender CLI with certificate

대한민국 목차 국명 지리 역사 정치 국방 경제 사회 문화 국제 순위 관련 항목 각주 외부 링크 둘러보기 메뉴북위 37° 34′ 08″ 동경 126° 58′ 36″ / 북위 37.568889° 동경 126.976667°  / 37.568889; 126.976667ehThe Korean Repository문단을 편집문단을 편집추가해Clarkson PLC 사Report for Selected Countries and Subjects-Korea“Human Development Index and its components: P.198”“http://www.law.go.kr/%EB%B2%95%EB%A0%B9/%EB%8C%80%ED%95%9C%EB%AF%BC%EA%B5%AD%EA%B5%AD%EA%B8%B0%EB%B2%95”"한국은 국제법상 한반도 유일 합법정부 아니다" - 오마이뉴스 모바일Report for Selected Countries and Subjects: South Korea격동의 역사와 함께한 조선일보 90년 : 조선일보 인수해 혁신시킨 신석우, 임시정부 때는 '대한민국' 국호(國號) 정해《우리가 몰랐던 우리 역사: 나라 이름의 비밀을 찾아가는 역사 여행》“남북 공식호칭 ‘남한’‘북한’으로 쓴다”“Corea 대 Korea, 누가 이긴 거야?”국내기후자료 - 한국[김대중 前 대통령 서거] 과감한 구조개혁 'DJ노믹스'로 최단기간 환란극복 :: 네이버 뉴스“이라크 "韓-쿠르드 유전개발 MOU 승인 안해"(종합)”“해외 우리국민 추방사례 43%가 일본”차기전차 K2'흑표'의 세계 최고 전력 분석, 쿠키뉴스 엄기영, 2007-03-02두산인프라, 헬기잡는 장갑차 'K21'...내년부터 공급, 고뉴스 이대준, 2008-10-30과거 내용 찾기mk 뉴스 - 구매력 기준으로 보면 한국 1인당 소득 3만弗과거 내용 찾기"The N-11: More Than an Acronym"Archived조선일보 최우석, 2008-11-01Global 500 2008: Countries - South Korea“몇년째 '시한폭탄'... 가계부채, 올해는 터질까”가구당 부채 5000만원 처음 넘어서“‘빚’으로 내몰리는 사회.. 위기의 가계대출”“[경제365] 공공부문 부채 급증…800조 육박”“"소득 양극화 다소 완화...불평등은 여전"”“공정사회·공생발전 한참 멀었네”iSuppli,08年2QのDRAMシェア・ランキングを発表(08/8/11)South Korea dominates shipbuilding industry | Stock Market News & Stocks to Watch from StraightStocks한국 자동차 생산, 3년 연속 세계 5위자동차수출 '현대-삼성 웃고 기아-대우-쌍용은 울고' 과거 내용 찾기동반성장위 창립 1주년 맞아Archived"중기적합 3개업종 합의 무시한 채 선정"李대통령, 사업 무분별 확장 소상공인 생계 위협 질타삼성-LG, 서민업종인 빵·분식사업 잇따라 철수상생은 뒷전…SSM ‘몸집 불리기’ 혈안Archived“경부고속도에 '아시안하이웨이' 표지판”'철의 실크로드' 앞서 '말(言)의 실크로드'부터, 프레시안 정창현, 2008-10-01“'서울 지하철은 안전한가?'”“서울시 “올해 안에 모든 지하철역 스크린도어 설치””“부산지하철 1,2호선 승강장 안전펜스 설치 완료”“전교조, 정부 노조 통계서 처음 빠져”“[Weekly BIZ] 도요타 '제로 이사회'가 리콜 사태 불러들였다”“S Korea slams high tuition costs”““정치가 여론 양극화 부채질… 합리주의 절실””“〈"`촛불집회'는 민주주의의 질적 변화 상징"〉”““촛불집회가 민주주의 왜곡 초래””“국민 65%, "한국 노사관계 대립적"”“한국 국가경쟁력 27위‥노사관계 '꼴찌'”“제대로 형성되지 않은 대한민국 이념지형”“[신년기획-갈등의 시대] 갈등지수 OECD 4위…사회적 손실 GDP 27% 무려 300조”“2012 총선-대선의 키워드는 '국민과 소통'”“한국 삶의 질 27위, 2000년과 2008년 연속 하위권 머물러”“[해피 코리아] 행복점수 68점…해외 평가선 '낙제점'”“한국 어린이·청소년 행복지수 3년 연속 OECD ‘꼴찌’”“한국 이혼율 OECD중 8위”“[통계청] 한국 이혼율 OECD 4위”“오피니언 [이렇게 생각한다] `부부의 날` 에 돌아본 이혼율 1위 한국”“Suicide Rates by Country, Global Health Observatory Data Repository.”“1. 또 다른 차별”“오피니언 [편집자에게] '왕따'와 '패거리 정치' 심리는 닮은꼴”“[미래한국리포트] 무한경쟁에 빠진 대한민국”“대학생 98% "외모가 경쟁력이라는 말 동의"”“특급호텔 웨딩·200만원대 유모차… "남보다 더…" 호화病, 고질병 됐다”“[스트레스 공화국] ① 경쟁사회, 스트레스 쌓인다”““매일 30여명 자살 한국, 의사보다 무속인에…””“"자살 부르는 '우울증', 환자 중 85% 치료 안 받아"”“정신병원을 가다”“대한민국도 ‘묻지마 범죄’,안전지대 아니다”“유엔 "학생 '성적 지향'에 따른 차별 금지하라"”“유엔아동권리위원회 보고서 및 번역본 원문”“고졸 성공스토리 담은 '제빵왕 김탁구' 드라마 나온다”“‘빛 좋은 개살구’ 고졸 취업…실습 대신 착취”원본 문서“정신건강, 사회적 편견부터 고쳐드립니다”‘소통’과 ‘행복’에 목 마른 사회가 잠들어 있던 ‘심리학’ 깨웠다“[포토] 사유리-곽금주 교수의 유쾌한 심리상담”“"올해 한국인 평균 영화관람횟수 세계 1위"(종합)”“[게임연중기획] 게임은 문화다-여가활동 1순위 게임”“영화속 ‘영어 지상주의’ …“왠지 씁쓸한데””“2월 `신문 부수 인증기관` 지정..방송법 후속작업”“무료신문 성장동력 ‘차별성’과 ‘갈등해소’”대한민국 국회 법률지식정보시스템"Pew Research Center's Religion & Public Life Project: South Korea"“amp;vwcd=MT_ZTITLE&path=인구·가구%20>%20인구총조사%20>%20인구부문%20>%20 총조사인구(2005)%20>%20전수부문&oper_YN=Y&item=&keyword=종교별%20인구& amp;lang_mode=kor&list_id= 2005년 통계청 인구 총조사”원본 문서“한국인이 좋아하는 취미와 운동 (2004-2009)”“한국인이 좋아하는 취미와 운동 (2004-2014)”Archived“한국, `부분적 언론자유국' 강등〈프리덤하우스〉”“국경없는기자회 "한국, 인터넷감시 대상국"”“한국, 조선산업 1위 유지(S. Korea Stays Top Shipbuilding Nation) RZD-Partner Portal”원본 문서“한국, 4년 만에 ‘선박건조 1위’”“옛 마산시,인터넷속도 세계 1위”“"한국 초고속 인터넷망 세계1위"”“인터넷·휴대폰 요금, 외국보다 훨씬 비싸”“한국 관세행정 6년 연속 세계 '1위'”“한국 교통사고 사망자 수 OECD 회원국 중 2위”“결핵 후진국' 한국, 환자가 급증한 이유는”“수술은 신중해야… 자칫하면 생명 위협”대한민국분류대한민국의 지도대한민국 정부대표 다국어포털대한민국 전자정부대한민국 국회한국방송공사about korea and information korea브리태니커 백과사전(한국편)론리플래닛의 정보(한국편)CIA의 세계 정보(한국편)마리암 부디아 (Mariam Budia),『한국: 하늘이 내린 한 폭의 그림』, 서울: 트랜스라틴 19호 (2012년 3월)대한민국ehehehehehehehehehehehehehehWorldCat132441370n791268020000 0001 2308 81034078029-6026373548cb11863345f(데이터)00573706ge128495

Cannot Extend partition with GParted The 2019 Stack Overflow Developer Survey Results Are In Announcing the arrival of Valued Associate #679: Cesar Manara Planned maintenance scheduled April 17/18, 2019 at 00:00UTC (8:00pm US/Eastern) 2019 Community Moderator Election ResultsCan't increase partition size with GParted?GParted doesn't recognize the unallocated space after my current partitionWhat is the best way to add unallocated space located before to Ubuntu 12.04 partition with GParted live?I can't figure out how to extend my Arch home partition into free spaceGparted Linux Mint 18.1 issueTrying to extend but swap partition is showing as Unknown in Gparted, shows proper from fdiskRearrange partitions in gparted to extend a partitionUnable to extend partition even though unallocated space is next to it using GPartedAllocate free space to root partitiongparted: how to merge unallocated space with a partition