Chinese Hypersonic Developments (HGVs/HCMs)

Nx4eu

Nx4eu

Junior Member
Registered Member
yugocrosrb95 said:
For the record, Fattah-1 exists, made and been used by Iran.

Yes, Iran does not have HGV with such propulsion yet does not mean their HGV is not powered simply due to not being air breathing.
If we go by your personal opinion as a standard then P-15 is not a cruise missile because it is solely powered by rocket motor.
Though North Korea and Iran made P-15 derivative that replaces liquid fuel rocket motor propulsion with air breathing turbojet engine.

As you said it yourself, it is your belief, does not make it a fact just as for example flat earthers say Earth is flat and not round.

If it was simply a MaRV then HGV of Fattah-1 would not have contained solid fuel rocket motor to begin with.
Depending on use case to extend range, conduct endo-atmospheric maneuvers or reduce loss of velocity during atmospheric reentry.

As you said it yourself, your opinion just as is on Fattah-1 for which you deny it being powered despite fact it has rocket motor/engine.

You mention those not in here which is odd to do, also you are welcome to believe whatever you want as long you keep it to yourself.
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Why are you two still arguing about Iranian missiles when this is the

Chinese Hypersonic Developments (HGVs/HCMs) thread???​

Especially after a mod has already asked you guys to stop. Stop polluting the thread with nonsense.
 
M

Mboxes

Just Hatched
Registered Member
ismellcopium said:
¿Quién dice que el alcance del YJ-17 es de solo 1000 km? ¡Qué risa!
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.I don't really know the range; I thought all those anti-ship missiles in the September parade had a range of 500 to 1000 km. I'm not a military expert, just an enthusiast. Cheers.
 
M

Mboxes

Just Hatched
Registered Member
CMP said:
El alcance estimado debe ser de hasta 2000 km, pero no menos de 1500.
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.Impressive , because the size of those missiles is small or medium for that range, now they are new generation, not like the cold war.
 
A

anzha

Captain
Registered Member
Experimental and numerical study on clustering characteristics of flame spatio-temporal evolution during ignition process induced by ignitor position in a central sudden expansion supersonic combustor

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The influence of the periodic longitudinal concentration gradient on the detonation re-initiation behind the pre-detonation tube

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Active and passive drag reduction methods for supersonic internal flow paths in combined cycle engines

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