Volna

R-29R designed by State Rocket Center Makayev and related to the Shtil' Launch Vehicle . The Volna is a 3-stage launch vehicle that uses liquid propellant. The warhead section is used for the payloads that can be either put into orbit with the help of an additional boost engine or travel along a sub-orbital trajectory to be recovered at the landing site. Volna can be launched from Delta III-class submarine

or from land based facilities.

Performance

Because of its mobile launch platform the Volna launch vehicle can reach a large number of different inclinations and could increase its performance to low Earth orbit by launching from equatorial sites. All flights to date have taken place from the Barents Sea. From this site the Volna can lift 100 kg (220 lb) into a 400 km (250 mi) high orbit with an inclination of 79°.^{[citation needed]} The warhead section can accommodate a payload of up to 1.3 m³ (46 cu ft). For sub-orbital missions the payload can be either a recoverable vehicle of up to 720 kg (1,590 lb) or research equipment placed in a descent vehicle of up to 400 kg (880 lb).^{[citation needed]}

Launch history

The first launch of the Volna took place at June 6, 1995 on a suborbital trajectory. The payload of this flight was a thermal-convectional Earth model developed by Bremen University (Germany).
On 20 July 2001 the second flight took place with a simplified (two-bladed) test vehicle of the
Delta III Submarine Borisoglebsk in the Barents Sea. Although the launch vehicle reached the intended suborbital trajectory the spacecraft failed to separate. The separation command was not issued by the flight software because of the presence of non-nominal variations. Failure of the Cosmos-1 to separate also resulted in the loss of the secondary payload, a new inflatable re-entry vehicle.^[1]^[2]

On 12 July 2002 the Volna was used for a sub-orbital flight for a second attempt to test a new re-entry vehicle, IRDT-2. The launch took place from

Delta III class submarine

K-44 Ryazan. Due to a failure in the launcher/payload interface the vehicle was lost and did not land on the expected area on the Kamchatka peninsula. It is unclear whether the spacecraft separated from the third stage of the Volna and did not inflate correctly or that it remained attached to the payload module. Remains of the vehicle have not been found.

The fourth flight took place at 21 June 2005 with on board the
Delta III Submarine Borisoglebsk in the Barents Sea. The spacecraft failed to reach orbit after stage one shut down prematurely at 82.86 seconds instead of the expected 100 seconds. The failure was attributed to “critical degradation in operational capability of the engine turbo-pump”. The second and third stage did not separate and the payload did not reach orbit.^{[citation needed}
]

On 6 October 2005 the Volna carried IRDT-2R on a sub-orbital trajectory, launched from Delta III Class Submarine Borisoglebsk in the Barents Sea. The launch vehicle performed nominally and placed the payload on a trajectory towards the Kamchatka peninsula. Trajectory data shows that the vehicle most likely overshot the landing site and could not be recovered.

References

^ "Cosmos Test". Gunter's Space Page. Retrieved 2016-07-09.
^ "Russia jumps on the inflatable bandwagon". RussianSpaceWeb. Retrieved 2016-07-09.

External links

[1] "Cosmos Test". Gunter's Space Page. Retrieved 2016-07-09.

[2] "Russia jumps on the inflatable bandwagon". RussianSpaceWeb. Retrieved 2016-07-09.

[1]

[2]

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS ^† Kaituozhe 2 Kinetica-1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H LVM3 Minotaur I IV V C Nuri OS-M1 ^† Pegasus XL Proton-M PSLV Qaem 100 Qased RS1 ^† Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega original C Vulcan Centaur Zenit 3SL 3SLB 3F Zhuque 2
In development	Antares 330 Ariane 6 Bloostar Cyclone-4M Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 12 Miura 5 MLV Neutron New Glenn New Line 1 NGLV OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan ^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard VLS-1^† Zenit 2 2M 2FG Zhuque 1 ^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

Performance

Launch history

See also

References

External links