NK-33

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NK-33
Aerojet AJ26 in the Stennis E-1 Test Stand - cropped.jpg
The Russian NK-33 was modified and renamed the AJ26-58 by Aerojet. This AJ26-58 is shown during a test firing at John C. Stennis Space Center
Country of origin Soviet Union
Date 1970s
Designer Kuznetsov Design Bureau
Application 1st/2nd stage engine
Predecessor NK-15, NK-15V
Successor AJ26-58, AJ26-59, AJ26-62
Liquid-fuel engine
Propellant LOX / kerosene
Cycle Staged combustion
Pumps Turbopump
Performance
Thrust (vac.) 1,680 kN (380,000 lbf)
Thrust (SL) 1,510 kN (340,000 lbf)
Throttle range 50%-105%
Thrust-to-weight ratio 137
Chamber pressure 14.83 MPa (2,151 psi)
Isp (vac.) 331 seconds (3.25 km/s)
Isp (SL) 297 seconds (2.91 km/s)
Dimensions
Length 3.7 m (12 ft)
Diameter 2 m (6 ft 7 in)
Dry weight 1,240 kg (2,730 lb)
References
References [1]

The NK-33 and NK-43 are rocket engines designed and built in the late 1960s and early 1970s by the Kuznetsov Design Bureau. The NK designation is derived from the initials of chief designer Nikolay Kuznetsov. NK-33 was among the most powerful LOX/RP-1 rocket engines when it was built, with a high specific impulse and low structural mass. They were intended for the ill-fated Soviet N-1 rocket moon shot. NK-33A engine is now used on the first stage of the Soyuz-2-1v launch vehicle.

Design[edit]

The NK-33 series engines are high-pressure, regeneratively cooled staged combustion cycle bipropellant rocket engines, and use oxygen-rich preburners to drive the turbopumps. The turbopumps require subcooled liquid oxygen (LOX) to cool the bearings.[2][3] These kinds of burners are highly unusual, since their hot, oxygen-rich exhaust tends to attack metal, causing burn-through failures. The United States had not investigated oxygen-rich combustion technologies until the Integrated Powerhead Demonstrator project in the early 2000s.[4] The Soviets, however, perfected the metallurgy behind this method. The nozzle was constructed from corrugated metal, brazed to an outer and inner lining, giving a simple, light, but strong structure. In addition, since the NK-33 uses LOX and RG-1 as propellants, which have similar densities, a single rotating shaft could be used for both turbopumps.[5][not in citation given] The NK-33 engine is among the highest thrust-to-weight ratio of any Earth-launchable rocket engine, only NPO Energomash RD-253 and SpaceX Merlin 1D engine achieve a higher ratio. The specific impulse of the NK-33 is significantly higher than both these engines. The NK-43 is similar to the NK-33, but is designed for an upper stage, not a first stage. It has a longer nozzle, optimized for operation at altitude, where there is little to no ambient air pressure. This gives it a higher thrust and specific impulse, but makes it longer and heavier. It has a thrust-to-weight ratio of about 120:1.[6]

The predecessors of NK-33 and NK-43 are the earlier NK-15 and NK-15V engines, respectively.

The oxygen-rich technology lives on in the RD-170/-171 engines, their RD-180, and recently developed RD-191 derivatives, but these engines have no direct connection to the NK-33.

History[edit]

N-1[edit]

The N-1 launcher originally used NK-15 engines for its first stage, and a high-altitude modification (NK-15V) in its second stage. After four consecutive launch failures and no successes, the project was cancelled. While other aspects of the vehicle were being modified or redesigned, Kuznetsov improved his contributions into the NK-33 and NK-43, respectively.[7] The 2nd-generation vehicle was to be called the N-1F. By this point the Moon race was long lost, and the Soviet space program was looking to the Energia as its heavy launcher. No N-1F ever reached the launch pad.[8]

When the N-1 program was shut down, all work on the project was ordered destroyed. A bureaucrat instead took the engines, worth millions of dollars each, and stored them in a warehouse. Word of the engines eventually spread to America. Nearly thirty years after they were built, disbelieving rocket engineers were led to the warehouse. One of the engines was later taken to America, and the precise specification of the engine was demonstrated on a test stand.[8]

About 150 engines survived, and in the mid-1990s, Russia sold 36 engines to Aerojet General for $1.1 million each. This company also acquired a license for the production of new engines. Aerojet has modified and renamed the updated NK-33 to AJ26-58 and AJ26-62, and NK-43 to AJ26-59.[9][10] [11]

Kistler K-1[edit]

Kistler Aerospace, later called Rocketplane Kistler (RpK), designed their K-1 rocket around three NK-33s and an NK-43. On August 18, 2006, NASA announced that RpK had been chosen to develop Commercial Orbital Transportation Services for the International Space Station. The plan called for demonstration flights between 2008 and 2010. RpK would have received up to $207 million if they met all NASA milestones,[12][13][14] but on September 7, 2007, NASA issued a default letter warning that it would terminate the COTS agreement with Rocketplane Kistler in 30 days because RpK had not met several contract milestones.[15]

Antares[edit]

An Antares rocket being rolled out for testing, showing the two NK-33 engines.

The initial version of the Orbital Sciences Antares light-to-medium-lift launcher had two modified NK-33 in the first stage, a solid Castor 30-based second stage and an optional solid or hypergolic third stage.[16] The NK-33s were imported from Russia to the United States, modified, and re=designated as Aerojet AJ26s. This involved removing some electrical harnessing, adding U.S. electronics, qualifying it for U.S. propellants, and modifying the steering system.[17]

In 2010 stockpiled NK-33 engines were successfully tested for use by the Orbital Sciences Antares light-to-medium-lift launcher.[17] The Antares rocket was successfully launched from NASA's Wallops Flight Facility on April 21, 2013. This marked the first successful launch of the NK-33 heritage engines built in early 1970s.[18]

Aerojet agreed to recondition sufficient NK-33s to serve Orbital's 16-flight NASA Commercial Resupply Services contract. Beyond that, it had a stockpile of 23 1960s and 1970s era engines. Kuznetsov no longer manufactures the engines, so Orbital sought to buy RD-180 engines. Because NPO Energomash's contract with United Launch Alliance prevented this, Orbital sued ULA alleging anti-trust violations.[19] Aerojet offered to work with Kuznetsov to restart production of new NK-33 engines, to assure Orbital of an ongoing supply.[20] However, manufacturing defects in the engine's liquid oxygen turbopump and design flaws in the hydraulic balance assembly and thrust bearings were proposed as two possible causes[21] of the 2014 Antares launch failure. As announced on 5 November 2014, Orbital decided to drop the AJ-26 first stage from the Antares and source an alternative engine. On December 17, 2014, Orbital Sciences announced that it would use the NPO Energomash RD-181 on second-generation Antares launch vehicles and had contracted directly with NPO Energomash for up to 60 RD-181 engines. Two engines are used on the first stage of the current Antares.[22]

On May 13, 2014, Russian Deputy Prime Minister Dmitry Rogozin announced that Russia would no longer supply rocket engines for U.S. military launches, amid tensions arising from the 2014 Russian military intervention in Ukraine.[23]

Current and proposed uses[edit]

RSC Energia is proposing an "Aurora-L.SK" launch vehicle, which would use an NK-33 to power the first stage and a Blok DM-SL for the second stage.[24]

Soyuz-2-1v[edit]

In the early 2010s the Soyuz launch vehicle family was retrofitted with the NK-33 engine – using the lower weight and greater efficiency to increase payload; the simpler design and use of surplus hardware might actually reduce cost.[25] TsSKB-Progress uses the NK-33 as the first-stage engine of the lightweight version of the Soyuz rocket family, the Soyuz-2-1v.[26] The NK-33A intended for the Soyuz-2-1v was successfully hot-fired on 15 January 2013,[27] following a series of cold-fire and systems tests of the fully assembled Soyuz-1 in 2011–2012.[28] The NK-33 powered rocket was finally designated Soyuz-2-1v, with its maiden flight having taken place on 28 December 2013. One NK-33 engine replaces the Soyuz's central RD-108, with the four boosters of the first stage omitted – a version of the Soyuz rocket with four boosters powered by NK-33 engines (with one engine per booster) is as of 2015 not realized, which results in a reduced payload compared to the Soyuz-2 launch vehicle.

Versions[edit]

During the years there have been many versions of this engine:

  • NK-15 (GRAU index 11D51): Initial version for the N1 first stage.
  • NK-15V (GRAU index 11D52): Modified NK-15 optimized for vacuum operation, used on the N1 second stage.
  • NK-33 (GRAU index 11D111): Improved version for the N1F first stage, never flown.
  • NK-43 (GRAU index 11D112): Vacuum-optimized NK-33 for the N1F second stage, never flown.
  • AJ26-58 and AJ26-59: Modified NK-33 by Aerojet Rocketdyne. Planned used on the Kistler K-1.
  • AJ26-62: Modified NK-33 with additional gimbal mechanism by Aerojet Rocketdyne. Used on the Antares 100-series first stage.
  • NK-33A (GRAU index 14D15): Refurbished NK-33. Used on the Soyuz-2-1v first stage.
  • NK-33-1: Uprated NK-33 with gimbal mechanism. Planned used on the Soyuz-2.3 core stage.

Gallery[edit]

See also[edit]

References[edit]

  1. ^ "LRE NC-33 (11D111) and NC-43 (11D112)" (in Russian). Retrieved 1 April 2015. 
  2. ^ "Soyuz 2-1v". spaceflight101.net. Retrieved 18 March 2016. 
  3. ^ "Orbital ATK ready for Antares’ second life". NASASpaceflight. Retrieved 18 March 2016. 
  4. ^ U.S. Air Force-NASA Technology Demonstrator Engine for Future Launch Vehicles Successfully Fired During Initial Full Duration Test
  5. ^ Astronautix NK-33 entry
  6. ^ Astronautix NK-43 entry
  7. ^ Lindroos, Marcus. The Soviet Manned Lunar Program Massachusetts Institute of Technology. Accessed: 4 October 2011.
  8. ^ a b Clifton, Dan (2001-03-01). "The Engines That Came in from the Cold". Channel 4 (London). Ideal World Productions. Retrieved 2014-01-03. 
  9. ^ "Space Lift Propulsion". Aerojet. April 2011. 
  10. ^ Clark, Stephen (2010-12-19). "Taurus 2 main engine passes gimbal steering test". Spaceflight Now (Tonbridge, Kent, UK). Archived from the original on 2014-01-03. Retrieved 2014-01-03. 
  11. ^ "NK-33". Mark Wade (Encyclopedia Astronautica). 
  12. ^ "NASA selects crew, cargo launch partners". Spaceflight Now. August 18, 2006. 
  13. ^ "NASA Selects Crew and Cargo Transportation to Orbit Partners". SpaceRef. August 18, 2006. 
  14. ^ Alan Boyle (August 18, 2006). "SpaceX, Rocketplane win spaceship contest". MSNBC. 
  15. ^ "RpK's COTS Contract Terminated" (Press release). Aviation Week. 2007-09-10. Retrieved 2007-09-10. 
  16. ^ "Antares" (PDF). Orbital. 
  17. ^ a b Clark, Stephen (March 15, 2010). "Aerojet confirms Russian engine is ready for duty". Spaceflight Now. Archived from the original on 2013-08-13. Retrieved 2010-03-18. 
  18. ^ Bill Chappell (21 April 2013). "Antares Rocket Launch Is A Success, In Test Of Orbital Supply Vehicle". NPR. 
  19. ^ Dan Leone (June 24, 2013). "Orbital Sues ULA, Seeks RD-180 Engines, $515 Million in Damages". Space News. 
  20. ^ Amy Butler (24 June 2013). "Orbital Frustrated By Lack Of Antares Engine Options". Aviation Week and Space Technology. 
  21. ^ Clark, Stephen (November 1, 2015). "Two Antares failure probes produce different results". Spaceflight Now. Retrieved 2015-11-01. 
  22. ^ Morring, Frank, Jr. (16 December 2014). "Antares Upgrade Will Use RD-181s In Direct Buy From Energomash". Aviation Week. Retrieved 28 December 2014. 
  23. ^ Ratnam, Gopal (13 May 2014). "Russia Bans Rocket Engine Sales to U.S. Military". Bloomberg. 
  24. ^ "S.P.Korolev RSC Energia - LAUNCHERS". Energia. 
  25. ^ "The Soyuz 1 (Soyuz 2-1v) Rocket". Russian Space Web. November 2010. 
  26. ^ Zak, Anatoly. "The Soyuz-1 rocket". Russian Space Web. Retrieved 7 March 2010.  External link in |publisher= (help)
  27. ^ "NK-33 Engine Test Successful" (in Russian). Samara Today. Retrieved January 2013. 
  28. ^ http://www.kosmonavtika.com/lanceurs/soyouz/version/14A15/14A15.html

External links[edit]