Volga (rocket stage): Difference between revisions
Content deleted Content added
m →top |
No edit summary Tags: Mobile edit Mobile web edit |
||
| (7 intermediate revisions by 7 users not shown) | |||
| Line 1: | Line 1: | ||
{{Infobox rocket stage |
{{Infobox rocket stage |
||
|name = Volga<ref>{{cite web|title=Volga upper stage|url=http://russianspaceweb.com/volga.html|website=Russianspaceweb.com| |
|name = Volga<ref>{{cite web|title=Volga upper stage|url=http://russianspaceweb.com/volga.html|website=Russianspaceweb.com|access-date=10 March 2016}}</ref> |
||
|manufacturer = [[TsSKB-Progress]] |
|manufacturer = [[TsSKB-Progress]] |
||
|country-origin = |
|country-origin = Russia |
||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
|length = {{convert|1.025|m}} |
|length = {{convert|1.025|m}} |
||
|diameter = {{convert|3.2|m}} |
|diameter = {{convert|3.2|m}} |
||
|propmass = {{convert|300|-|900|kg}} |
|propmass = {{convert|300|-|900|kg}} |
||
|empty = {{convert|840|kg}} |
|empty = {{convert|840|kg}} |
||
{{Infobox rocket/stage |
|||
| name = Volga |
|||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
}} |
}} |
||
}} |
|||
'''Volga''', [[GRAU index]] 14S46, also designated 141KS, is a rocket [[upper stage]] designed in |
'''Volga''', [[GRAU index]] '''14S46''', also designated '''141KS''', is a rocket [[upper stage]] designed in Russia. It is used with the [[Soyuz-2 (rocket)|Soyuz-2.1a]] and [[Soyuz-2-1v]] rockets to insert payloads into [[Sun-synchronous orbit]]. It is derived from the propulsion module of the [[Yantar (satellite)|Yantar]] [[spy satellite]]s.<ref>{{cite web|title=Soyuz 2-1v Launch Vehicle|url=http://spaceflight101.com/spacerockets/soyuz-2-1v/|website=Spaceflight101|access-date=26 March 2016}}</ref> It is closely related to the retired [[Ikar (rocket stage)|Ikar upper stage]].<ref name="nsf-20160427">{{Cite web|url=https://www.nasaspaceflight.com/2016/04/vostochny-maiden-soyuz-launch/|title=Soyuz 2-1 launches maiden mission from Vostochny {{!}} NASASpaceFlight.com|website=www.nasaspaceflight.com|date=27 April 2016 |access-date=2016-05-01}}</ref> |
||
== References == |
== References == |
||
| Line 19: | Line 22: | ||
{{Upper stages}} |
{{Upper stages}} |
||
| ⚫ | |||
[[Category:Expendable space launch systems]] |
[[Category:Expendable space launch systems]] |
||
[[Category:Rocket stages]] |
[[Category:Rocket stages]] |
||
[[Category:Space launch vehicles of Russia]] |
[[Category:Space launch vehicles of Russia]] |
||
| ⚫ | |||
Latest revision as of 15:12, 22 May 2024
| Manufacturer | TsSKB-Progress |
|---|---|
| Country of origin | Russland |
| General characteristics | |
| Diameter | 3.2 metres (10 ft) |
| Length | 1.025 metres (3 ft 4.4 in) |
| Propellant mass | 300–900 kilograms (660–1,980 lb) |
| Empty mass | 840 kilograms (1,850 lb) |
| Volga | |
| Powered by | 1x 17D64[2][3] (KB Melnikov) |
| Maximum thrust | 2.94 kilonewtons (660 lbf) |
| Specific impulse | 307 seconds (3.01 km/s) |
| Burn time | 600 s |
| Propellant | N2O4/UDMH |
Volga, GRAU index 14S46, also designated 141KS, is a rocket upper stage designed in Russia. It is used with the Soyuz-2.1a and Soyuz-2-1v rockets to insert payloads into Sun-synchronous orbit. It is derived from the propulsion module of the Yantar spy satellites.[4] It is closely related to the retired Ikar upper stage.[3]
References
[edit]- ^ "Volga upper stage". Russianspaceweb.com. Retrieved 10 March 2016.
- ^ "Soyuz-2-1v Launcher (formerly Soyuz-1)". Retrieved 26 March 2016.
- ^ a b "Soyuz 2-1 launches maiden mission from Vostochny | NASASpaceFlight.com". www.nasaspaceflight.com. 27 April 2016. Retrieved 2016-05-01.
- ^ "Soyuz 2-1v Launch Vehicle". Spaceflight101. Retrieved 26 March 2016.
 | This rocketry article is a stub. You can help Wikipedia by expanding it. |