RL10: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
Rescuing 2 sources and tagging 0 as dead.) #IABot (v2.0.8 |
Rescuing 1 sources and tagging 0 as dead.) #IABot (v2.0.8 |
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Baris 250:
; RL10B-2 Specifications
* Thrust (altitude): 24,750 lbf (110.1 kN)<ref name=pwr_rl10b-2.pdf>{{cite web |url=http://www.pw.utc.com/products/pwr/assets/pwr_rl10b-2.pdf |title=RL10B-2 |publisher=[[Pratt & Whitney Rocketdyne]] |date=2009 |accessdate=January 29, 2012 |archive-date=2012-03-26 |archive-url=https://web.archive.org/web/20120326211303/http://www.pw.utc.com/products/pwr/assets/pwr_rl10b-2.pdf |dead-url=yes }}</ref>
* Design: [[Expander cycle (rocket)|Expander cycle]]<ref name="">{{cite journal |url=http://www.dtic.mil/cgi-bin/GetTRDoc?AD=ADA397948 |title=50K expander cycle engine demonstration |journal=AIP Conference Proceedings |first1=A M |last1=Sutton |first2=S D |last2=Peery |first3=A B |last3=Minick |volume=420 |pages=pp. 1062–1065 |date=January 1998 |doi=10.1063/1.54719}}</ref>
* [[Specific impulse]]: {{convert|464|isp}}<ref name=pwr_rl10b-2.pdf />
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