Wahana peluncur antariksa: Perbedaan antara revisi

Konten dihapus Konten ditambahkan
Rotlink (bicara | kontrib)
k fixing dead links
Rotlink (bicara | kontrib)
k fixing dead links
Baris 1.533:
| {{USA}}
| [[SpaceX]]
| {{nts|53000}}<ref name=sxFH20130322>{{cite web |title=Falcon Heavy Overview|url=https://spacex.com/falcon_heavy.php |date=2013<!-- SpaceX copyright on the web page --> |publisher=SpaceX |accessdate=2013-03-22}}</ref><ref name="SpaceX">{{cite web |title=SpaceX Brochure |url= http://www.spacex.com/downloads/spacex-brochure.pdf|publisher=Spacex.com |accessdate=14 June 2011|archiveurl=http://web.archive.org/web/20100107075247/http://www.spacex.com/downloads/spacex-brochure.pdf|archivedate=7 January 2010}}</ref>
| {{nts|12000}} to GTO<ref name=sxFH20130322/><br/>{{nts|16000}} to TLI<ref name="SpaceX"/>
| {{nts|83}}–128<ref name=sxFH20130322/><!-- "Pricing: Payloads up to 6.4 ton to GTO: $83M*; greater than 6.4 ton to GTO $128M* ... *Paid in full standard launch prices for 2012" --><!-- these published prices are explicitly listed on the 2013 version of the FH web page at SpaceX, but are listed as "launch prices for 2012"; the older/somewhat lower numbers that had been claimed have no source provided at all. -->
Baris 1.702:
| [[Mitsubishi Heavy Industries]]
| {{nts|16500}}<ref name=sxFH20130322/>
| {{nts|8000}}<ref name="H-IIB_2">{{cite web| url= http://www.jaxa.jp/pr/brochure/pdf/01/rocket05.pdf | title=H-IIB Launch Vehicle, P. 2 | publisher=[[Jaxa]] | accessdate=3 September 2008|archiveurl=http://web.archive.org/web/20090730201604/http://www.jaxa.jp/pr/brochure/pdf/01/rocket05.pdf|archivedate=30 July 2009}}</ref>{{deadlink|date=March 2013}}
|
|
Baris 2.109:
|[[Orbital Sciences Corporation|Orbital]]
|{{nts|580}}<ref name=osc20120228>
{{cite web |url=http://www.orbital.com/NewsInfo/Publications/Minotaur_I_Fact.pdf |title=Minotaur I Space Launch Vehicle—Fact Sheet |year=2012 |work= |publisher=Orbital Sciences Corporation |accessdate=2012-02-28 |quote=''Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)'' |archiveurl=http://web.archive.org/web/20061018165506/http://www.orbital.com/NewsInfo/Publications/Minotaur_I_Fact.pdf|archivedate=2006-10-18}}</ref>
|
|
Baris 2.854:
| {{USA}}
| [[Orbital Sciences Corporation|Orbital]]
| {{nts|6000}}<ref name="ostug13_201104">{{cite web |url=http://www.orbital.com/NewsInfo/Publications/Taurus_II_Guide.pdf |format=PDF|title=Taurus II User’s Manual, Rev. 1.3 |publisher=Orbital |date = April 2010|accessdate = 2010-11-11|archiveurl=http://web.archive.org/web/20100509062344/http://www.orbital.com/NewsInfo/Publications/Taurus_II_Guide.pdf|archivedate=2010-05-09}}</ref>
| {{nts|1900}} to GTO<ref name="ostug13_201104"/>
|