| 词条 | Ikar (rocket stage) |
| 释义 |
|name = Ikar[1] |manufacturer = TsSKB-Progress |country-origin = Russia |diameter = {{convert|2.72|m}} |length = {{convert|2.59|m}} |empty = {{convert|2310|kg}} |mass = {{convert|3210|kg}} |engines = 1 17D61[2] (KB Melnikov) |thrust = {{convert|2.943|kN}} |SI = 308 sec |time = 600 seconds |fuel = N2O4/UDMH }} The Ikar was a rocket upper stage designed in Russia in 1999 to be used with the Soyuz 11A511U rocket as Soyuz-Ikar.[3] It was derived from the propulsion module of the Yantar spy satellites.[4] References1. ^{{cite web|title=IKAR Upper Stage|publisher=TsSKB-Progress|url=http://en.samspace.ru/products/upper_stages/bv_ikar/|accessdate=21 December 2015}} {{Upper stages}}{{Rocket-stub}}2. ^{{Cite web|url=http://www.cosmopark.ru/rb/5.html|title=Блок выведения 'Икар'|trans-title=Spacetug 'Ikar'|last=|first=|date=|website=www.cosmopark.ru|publisher=|language=Russian|access-date=2016-11-04}} 3. ^{{cite web |url=http://www.astronautix.com/lvs/soyuikar.htm |title=Soyuz 11A511U / Ikar |publisher=Astronautix.com |date= |accessdate=2012-09-04 |deadurl=yes |archiveurl=https://web.archive.org/web/20121005134352/http://astronautix.com/lvs/soyuikar.htm |archivedate=2012-10-05 |df= }} 4. ^{{cite web |url=http://www.astronautix.com/engines/17d61.htm |title=17D61 |publisher=Astronautix.com |date= |accessdate=2012-09-04 |deadurl=yes |archiveurl=https://web.archive.org/web/20121004194941/http://astronautix.com/engines/17d61.htm |archivedate=2012-10-04 |df= }} 3 : Expendable space launch systems|Rocket stages|Space launch vehicles of Russia |
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