This is a discussion on Behind the China Missile Hype within the Navy forums, part of the China Defense & Military category; Originally Posted by IronsightSniper 1. DF-21D is launched 2. It climbs to 500 km apogee 3. It's RV descends towards ...
Counter proposal
1. DF-21D is launched.
2. With mid course guidance, mid course correction is achieved to follow the CVBG. (Potential for mid course evasive maneuvers depending who you believe)
3. RV descends to where CVBG was last, by mid course guidance. Then mid course guidance turns off, terminal turns on.
4. Its onboard sensors detects, tracks and guides RV to the CVN.
The RV simply being shot at where the CV was last detected without mid course guidance and relying for its own relatively weak onboard sensors to search a large piece of ocean will be harder than using off board sensors (which already detected and tracked the CVBG in the first place) to track and send mid course correction to the missile and using the onboard sensors instead to have an easier job searching a much smaller piece of ocean, because it'll have been following the CVBG rather than the "radius" of which CVBG could have moved since DF-21D was fired.
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The difference is, as illustrated by analyses of the PLA's test of the DF-21D against the concrete slab, is that the carrier doesn't actually have much far to go.
I haven't bothered to calculate how long it takes a 3,000 km ranged missile like the DF-21D to go up and go down on a target around 3,000 km away, but assume it takes 30 minutes to do so, which is around the time it takes an ICBM to go around the globe and hit something. At 35 knots, the CV could have travelled 32.41 km in any direction. The terminal stage of the DF-21D most likely goes active relatively soon after it's terminal stage begins, which means it has the advantage of being able to scan a large swath of ocean in the first place. It doesn't need a rather powerful on-board sensor system, because it's a rather large on-board sensor system.
About mid-course guidance, of course, like we've concluded before, there's no proof for or against mid-course guidance anyways, so I'm not going to pursue an argument there.
Fair enough.
Though I think it would be strange if the sensor assets didn't assist in the guidance of weapon systems themselves, whether it be AShBM or the likes of YJ-62s or swarms of 022s with YJ-83s.
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Ok, more one the Pershing II :
Link
I posted this before I'll post it again : Technical Manual & Operator's Manual...Pershing II was launched from a M-790 flatbed trailer towed by a M-1001 prime mover. This had a max speed of 40mph and a road range of 450 miles. (To save money, only enough M-1001’s were bought for active units in Europe, stateside training units used existing HEMTT prime movers.) It was guided inertially through most of the flight. After atmospheric re-entry, the RADAG (Radar Digital Area Guidance) system took over. This took four successively-closer radar “snapshots” of the target as the MARV descended, giving the guidance computer a 128 square-pixel portrait to home on. In the event RADAG was jammed or failed, the Pershing II continued on inertial guidance. The warhead could be set for impact or airburst. The first and second rocket stages, essentially identical, were of a new design that used Kevlar and hybrid-alloy materials. Steering was by vanes in the exhaust in the atmosphere and a reactive system above it. The first stage separated at 1/3rd of the apogee altitude....
I also attached to screenshots from "Chapter 2 : Missile Description (2-9 to 2-16)"
Plus,
Off-course MGM-31C, Iskander-K/M, etc all are used against FIXED targets and not something that is moving. Hitting a something moving at 30kt making evasive moves....well thats different story
i'm sure china has defense against attacks. but how effective are against US strike and how many system does DF21 need, the more system required to support DF21, the more chance that system will be disabled by US. its matter of probability. and right now the odd is in favor of US due to its overall combat ability and equipments.
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some system require less support some require more. the more it require the more chance that part of system will be disable. if we look at overall capability of US force vs china, the odd is favoring US. if DF21 require OTH, Sub, satelite and other system, then disable any of these will reduce the DF21 threat signficanlly. in this case china has to spread its resource to cover all these system in order for DF21 to work. properly.
Counter counter proposal.
1. DF-21D is launched.
2. With mid course guidance, mid course correction is achieved to follow the CVBG. (Potential for mid course evasive maneuvers depending who you believe)
3. RV descends to an launch point away from the target area.
4. Release a number of AshCM (YJ-82 variants).
5. YJ-82s lit their turbofans, goes on to a search pattern with their own sensor active in target area. just like as if a frigate or fighterbomber launched those missiles.
and people in side of chinese aerospace industry has proposed this one time. (don't ask me how I know)
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As far as hot plasma in reentry phase preclude communication and use of radar.
I would like to point out that
1. not all phases of reentry does black out occure.
2. Pershin II does a pull up manuever towards the end to slow down and point its radar.
3. Iskander-E has a datalink. that is able to beam back pictures. as the warhead dives towards earth.
4. NASA and China National Space Adminstration both has data relay satellites (for NASA it is Tracking and Data Relay Satellite System)
that allowed for tracking and communication during "blackout".
basically the back end of re-entry vehicle has no obstruction by plasma.
Communications blackout - Wikipedia, the free encyclopedia
for CNSA the satellites are called Tianlian series, or "Sky link".
2nd Chinese Data Relay Satellite Reaches Orbit | SpaceNews.com
which was used on space docking mission this year.
this presumablly give them a similar capability as TDRSS gives nasa during shuttle reentry black out.
all of these are in geostationary orbits.
===
Therefore it is pretty safe to say that NikeX concerns are pretty much addressed.
How do you update the inertial guidance to hit a moving target? Your answer please.
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With the hot plasma surrounding the DF-21D RV how is this accomplished?
How does the DF-21D RV see through the hot plasma to detect the CVN and begin the terminal phase?
Again, how does the DF-21D RV communicate with the offboard sensors while surrounded by a hot plasma like this? How?
---------- Post added at 03:20 PM ---------- Previous post was at 03:01 PM ----------
During the critical period of DF-21 flight it does. The terminal phase
Pershing 2 uses another kind of radar guidance and Pershing 2 is engaging a FIXED target. Your example does not apply in the case of the DF-21D attempting to engage a MOVING target, the CVN
Oh and Pershing 2 used a NUCLEAR warhead. DF-21 is suppose to use a conventional explosive warhead
Warhead
W85 nuclear warhead: 5 kilotons of TNT (21 TJ) to 80 kilotons of TNT (330 TJ)
...Radar area correlator
The highly accurate terminal guidance technique used by the Pershing II RV was radar area correlation, using a Goodyear Aerospace active radar guidance system. This technique compared live radar video return to prestored reference scenes of the target area and determined RV position errors with respect to its trajectory and target location. These position errors were used to update the inertial guidance system, which in turn sent commands to the vane control system to guide the RV to the target.
During rentry phase of the flight plasma backout will occur. There will be no pictures or datalink beamed anywhere. Physics prevents datalinks
So DF-21D will have to be aligned with data relay satellites? Not likely to happen. Try again
I give you points for at least realizing that plasma blocks communications during re-entry of DF-21D RV
Mid course guidance/correction via data relay satellites the same principle as how ICBMs receive GPS data to increase accuracy.
the same way ICBMs receive GPS data mid flight. It'll only be in the re entry/terminal phase that "black outs" become a potentially bigger problemWith the hot plasma surrounding the DF-21D RV how is this accomplished?
And that has been solved by TRDSS as ie said
Tracking and Data Relay Satellite System - Wikipedia, the free encyclopedia
Communications blackout - Wikipedia, the free encyclopedia
Until the creation of the Tracking and Data Relay Satellite System (TDRSS), the Space Shuttle endured a 30-minute blackout. The TDRSS allowed the Shuttle to communicate by relay with a Tracking and Data Relay Satellite during re-entry, through a "hole" in the ionized air envelope at the tail end of the craft, created by the Shuttle's shapeThe same way Iskander/pershing ii's optical and active radar works. The point is that those two vastly different types of terminal guidance does work during high mach re entry. Logic tells me other types like MMW, anti radiation etc should work as well but that's another discussion.How does the DF-21D RV see through the hot plasma to detect the CVN and begin the terminal phase?
Data relay sats the same way space shuttle communicates with TDRSS during re entry.Again, how does the DF-21D RV communicate with the offboard sensors while surrounded by a hot plasma like this? How?
Even if there was a black out at that period it would be down to terminal guidance by that point anyway, and I've proven over and over again how high mach re entry doesn't effect terminal guidance (Iskander/pershing II)During the critical period of DF-21 flight it does. The terminal phase
Your argument is that the plasma from re entry will make the RV's terminal guidance useless, blinding it so to speak. Pershing II and Iskander have shown this is not true. The fact that DF-21D is engaging a moving target does not somehow make the plasma from re entry suddenly effect its own terminal guidance system.Pershing 2 uses another kind of radar guidance and Pershing 2 is engaging a FIXED target. Your example does not apply in the case of the DF-21D attempting to engage a MOVING target, the CVN
I do agree engaging a fixed and moving target is obviously different, but it has no influence on your so called plasma problem's effect on the DF-21Ds terminal guidance from Iskander/Pershing 2
How is the fact that pershing 2 was supposed to have a nuclear warhead relevant to the discussion? Is it relevant to the pershing 2's inherent accuracy or it's terminal guidance? No. So why mention it?Oh and Pershing 2 used a NUCLEAR warhead. DF-21 is suppose to use a conventional explosive warhead
Warhead
W85 nuclear warhead: 5 kilotons of TNT (21 TJ) to 80 kilotons of TNT (330 TJ)
...Radar area correlator
The highly accurate terminal guidance technique used by the Pershing II RV was radar area correlation, using a Goodyear Aerospace active radar guidance system. This technique compared live radar video return to prestored reference scenes of the target area and determined RV position errors with respect to its trajectory and target location. These position errors were used to update the inertial guidance system, which in turn sent commands to the vane control system to guide the RV to the target.
Yet somehow it works for Iskander... So either you're wrong or the Russians are lying to us. I wonder which it could be.During rentry phase of the flight plasma backout will occur. There will be no pictures or datalink beamed anywhere. Physics prevents datalinks
... And as you're so fond of copy/pasting paragraphs over and over again...
2nd Chinese Data Relay Satellite Reaches Orbit | SpaceNews.comUntil the creation of the Tracking and Data Relay Satellite System (TDRSS), the Space Shuttle endured a 30-minute blackout. The TDRSS allowed the Shuttle to communicate by relay with a Tracking and Data Relay Satellite during re-entry, through a "hole" in the ionized air envelope at the tail end of the craft, created by the Shuttle's shape.
So a solution's already here.China is the third nation, after the United States and Russia, to have its own manned space program, and the third to have an operational data-relay service. The U.S. Tracking and Data Relay Satellite System and Russia’s Loutch satellites perform similar data-relay functions, also from geostationary orbit.
I give you points for at least realizing there's an easy and existing way around your plasma problem which has existed for years. During this whole discussion I've mentioned data relay satellites what, a hundred times? I've said over and over again that AShBM won't work without data relay/mid course correction.So DF-21D will have to be aligned with data relay satellites? Not likely to happen. Try again
I give you points for at least realizing that plasma blocks communications during re-entry of DF-21D RV
Last edited by Bltizo; 02-10-2012 at 02:43 PM.
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I don't know because I'm not a part of the development of the ASBM. And I certainly know you don't know. You've shown you don't even know the basics. So what makes you think you know anything about this? Don't demand answers when you've not answered the majority of mine but instead spin or move on to another diversion.How do you update the inertial guidance to hit a moving target? Your answer please.
Thank you for that rare display of common sense. These words of yours represent the meat of the discussion:
"...the more system required to support DF21, the more chance that system will be disabled by US. its matter of probability..."
The more complex the kill chain the more that can go wrong. The Chinese DF-21D kill chain has several weak links. These links can be attacked.
If I were the Chinese and wanted to attack the carrier, I would top DF-21D with torpedoes and drop these NEAR the carrier and let the torpedoes do the homing
Something like SUBROC
... That would just be adding another layer of complexity because you'll have to get the missile to where the CVBG is anyway...
And you guys still don't get it do you? The C4ISR system which AShBM will rely on is not "and", it's "and/or". So if you shoot down one satellite it'll degrade the overall system to a degree but not disable it. And think about all the sensors which will make up this C4ISR -- satellites, UAVs, MPAs, fishing boats, OTH, submarines, sonar, PLAN ships, microsats. If you shoot down one of them it will degrade the overall system to a degree but will not disable the entire system as you say!
If you really wanted a "definitive" weak link to attack I suggest the data relay satellites. You won't ever able to disable all the sensors which make up C4ISR, but you can prevent the sensors from communicating with DF-21D in flight by destroying all the data relay sats. then it becomes a question of satellite vs ASAT, as well as the number of data relay satellites they have.
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Oh come on now. You do not have to be a member of the ASBM team to explain to us all the concepts for updating the inertial guidance system of a ballistic missile. There are stellar updates to name just one method. Dongfeng 31/A uses this method to improve accuracy
...
We were talking about attacking the DF-21D's C4ISR network, not attacking the RVs. Do you even know that you're changing the goalposts?
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Of course using stars to increase accuracy is one way of going about it -- it's one of the oldest, among long range ballistic missiles. My point was why did you ask the question if you knew the answer in the first place...
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