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Development of the NK-88 began in 1974 at the
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Otechestvennaya aviatsionno-kosmicheskaya tekhnika - SAMARSKIY NTK and ram-home.com
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flying laboratory. The other two nacelles contained engines of the native
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One NK-88 engine was tested in flight in the starboard nacelle of this
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2,300 kg (5,100 lb) (with heat exchanger and cryopump)
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two-spool low-bypass turbofan and was designed to run on
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was tested in flight in the starboard nacelle of the
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619:. If you have a source, you can help Knowledge by
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414:"NK-88 by Kuznetsov Engine Design Bureau"
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169:On April 15, 1988, one NK-88 running on
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225:Two-spool alternative fuel turbofan
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130:turbofan engine, designed by the
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281:103 kN (23,000 lbf)
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290:30 kg/(kN⋅h) in cruise on LH
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640:Low-bypass turbofan engines
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650:Kuznetsov aircraft engines
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314:Reaction Engines Scimitar
286:Specific fuel consumption
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326:List of aircraft engines
217:General characteristics
132:Kuznetsov Design Bureau
71:Kuznetsov Design Bureau
645:1980s turbofan engines
206:Specifications (NK-88)
160:liquified natural gas
126:was an experimental
303:Comparable engines
86:Major applications
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110:Developed into
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61:Soviet Union
621:adding them
269:Performance
252:Compressor:
239:Dry weight:
138:Development
634:Categories
530:Turboprops
332:References
257:Fuel type:
246:Components
162:(LNG) and
77:First run
477:Turbofans
466:Kuznetsov
423:8 October
395:8 October
234:Diameter:
211:Data from
201:(testbed)
173:stored LH
298:See also
275:Maximum
187:kerosene
164:kerosine
49:Turbofan
229:Length:
144:NK-8-2U
103:NK-8-2U
538:TV-022
520:NK-144
277:thrust
183:NK-8-2
22:NK-88
611:This
589:NK-93
584:NK-92
579:NK-89
574:NK-88
569:NK-14
553:NK-12
515:NK-87
510:NK-86
505:NK-32
500:NK-25
495:NK-22
223:Type:
156:NK-89
115:NK-89
45:Type
548:NK-4
543:TV-2
490:NK-8
485:NK-6
425:2021
397:2021
122:The
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150:(LH
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375:^
340:^
260:LH
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