Novator K-100: Perbedaan antara revisi

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k r2.5.4) (Robot: Mengubah en:Novator K-100 menjadi en:K-100 (missile)
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{{Infobox Weapon
|name = K-100-1
|image = [[Image:KS-172 NTW - 94.jpg|350px]]
|caption = Mockup of KS–172 in front of Su-30 in 1994
|origin = [[Russia]] & [[India]]
|type = air-to-air missile
<!-- Type selection -->
|is_missile=yes
<!-- Service history -->
|service =
|used_by =
|wars =
<!-- Production history -->
|designer =
|design_date =
|manufacturer = [[NPO Novator]] & [[DRDO]]
|unit_cost =
|production_date=
|number =
|variants =
<!-- General specifications -->
|spec_label=
|weight = {{convert|748|kg|lb|-1|abbr=on}}&nbsp;(KS–172)<ref name="Force" />
|length = {{convert|6.01|m|ft|abbr=on}} + {{convert|1.4|m|ft|abbr=on}}&nbsp;(KS–172)<ref name="Force" />
|diameter = {{convert|40|cm|in|abbr=on}}&nbsp;(KS–172)<ref name="Force" />
<!-- Explosive specifications -->
|filling= HE fragmentation&nbsp;(KS–172)<ref name="Force" />
|filling_weight= {{convert|50|kg|lb|-1|abbr=on}}
|detonation=
|yield=
<!-- Vehicle/missile specifications -->
|engine= Solid-propellant tandem rocket booster&nbsp;(KS–172)<ref name="Force" />
|engine_power=
|pw_ratio=
|transmission=
|payload_capacity=
|suspension=
|clearance=
|fuel_capacity=
|vehicle_range=At least 200km,<ref name="JDW" /> possibly 300–400&nbsp;km (160–210&nbsp;nmi)
|speed= {{convert|4000|km/h|mph|abbr=on|sigfig=2}}&nbsp;(KS–172)<ref name="Force" />
|guidance=[[inertial navigation]] with midcourse guidance and active radar for terminal homing&nbsp;(KS–172)<ref name="Force" />
|steering=
<!-- missiles only -->
|wingspan= {{convert|61|cm|in|abbr=on}}&nbsp;(KS–172)<ref name="Force" />
|propellant=
|ceiling=
|altitude={{convert|3|m|ft|abbr=on}}–{{convert|30000|m|ft|abbr=on}}&nbsp;(KS–172)<ref name="Force" />
|depth=
|boost=
|accuracy=
|launch_platform= [[Su-27]], [[Su-30]], [[Sukhoi Su-35|Su-35]],<ref name="Janes"/> [[Su-30MKI]]<ref name="Force" /> [[Sukhoi PAK FA|PAK FA]] (expected)
|transport=
}}
 
'''Novator K-100''' adalah rudal Rusia udara-ke-udara yang dirancang sebagai " AWACS killer " di rentang sampai 200 km. Rudal itu memiliki berbagai nama selama sejarah, termasuk Izdeliye 172 ('Article 172'), AAM-L ( RVV-L ), KS-172 , KS-1 , 172S-1 dan R-172 . Badan pesawat tampaknya telah berasal dari rudal permukaan-ke-udara (SAM) 9K37 Buk tetapi pembangunan terhenti pada pertengahan 1990-an karena kurangnya dana. Tampak pada tahun 2004 setelah kesepakatan dengan India, yang ingin menghasilkan rudal di India untuk Su-30MKI mereka .
 
== Referensi ==
{{Reflist}}
 
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[[Kategori:Peluru kendali udara ke udara]]