These costs were for tranche 2 examples which Austria ordered on 1 July 2003. 😉
Austria has a weird spec mix if I’m not mistaken. They didn’t license the RWR libraries and they didn’t buy PIRATE if I recall correctly.
Different levels of support, ToT and platform configuration make comparisons pretty difficult.
These costs were for tranche 2 examples which Austria ordered on 1 July 2003. 😉
Austria has a weird spec mix if I’m not mistaken. They didn’t license the RWR libraries and they didn’t buy PIRATE if I recall correctly.
Different levels of support, ToT and platform configuration make comparisons pretty difficult.
50% increase over a M.9 launch at 40k feet. If the F-15 is flying at the same speed and altitude, then there’d be no difference. The DIFFERENCE is what sort of fuel state will the F-15 be in to accelerate and climb, to match the F-22, and what sort of increase in IR signature will the use of A/B cause.
Could you put some more numbers to your example to explain the proposed 50% difference? What are your speed and height numbers for the baseline aircraft and what are your speed and height for the F-22?
Another thing in the food for thought category is that when these missiles are fired from a supercruising F-22 at high altitude, there’ll be another 50 percent increase due to the kinematic advantage.
50% increase according to which baseline? An F-15C going M1.6 at 40k ft?
Yes they were unused, but some time has passed since they were not delivered and nature does things to aircraft that make its interiors degrade.
Not just interiors. Pretty much any material degrades over time, and expecting an already 20-year-old airframe to get through its full service life of repeated stressing is rather optimistic.
Satorian,
Have you any idea how many notebooks I have? It’s only February, with no major shows, and I have five or six from this year. And have you seen my handwriting and abbreviations?
Today’s first entry reads:
OTR NFP as attrib ***** (AAIB) says BH precny grndg all 225. Tlbm (contns CVR + FDR) ny recvd.
Ex-Era 225 on lse. G-REDU????
Sea state? 1-2???
Hw dd floats inflate? H2O?
MR2 ‘R51’, HAR3A ‘R??’
3 pax(?) winched out of 1st LRft. Rest stayed in LRft B
A/C Fltd 5 hrs > Pissed abt waiting for safetyC? > sank (invtd???)
Cld craned onto deck by RH??? when still erect?
Call ***** ****** at *** re Jigsaw.
It makes sense to me, but to anyone else it’s gibberish
To say nothing of what possible gain there’d be in my making my hard-earned research easily available to anyone.
Sheesh, that reads like Ulysses.
Not saying you should make it immediately available. But there is a chance that all the information could be lost somewhere down the line, when it’s of no use to you anymore.
Unless you want to help feed future historians by giving them something to decipher. 🙂
will the Captor E look anything like this.
There are no details given. Just that the procurement is planned to start in 2012. The German MoD has to map out their financing plan five years in advance, and the Bundeswehrplan 2009 references that particular procurement plan.
No, they have the desire, & the intention. But it’s not urgent. They don’t need it – yet.
As of June 2008, the German Bundeswehr plans to procure Captor-E (as it is named in the addendum to the 2009 Bundeswehrplan) from 2012 on.
and the fact that it seems none of the 4 Typhoon main users have a strong desire to either integrate AESA, or fund further development of a real multi role standard since most of them still have good attack planes.
That’s not a fact, and as claim it’s wrong. 🙂
Germany has a “future obsolescence” fund and road map for the Eurofighter, where AESA is planned to be integrated on German Eurofighters.
As the article mentions, the Su-35BM material showed a similar “swashplate” arrangement. Looks interesting.
Seeing as how the GAF already has the money set aside to procure AESA radars for its Eurofighters, I guess we might see this design in service sometime in the future.
Couldn’t you accelerate the missile greatly initially, which as far as I know is the main point of ASRAAM. Changing it into a guided bullit in some respect.
Would it be worth it though? Aero drag = diminishing returns to increased initial power. Linear power development seems preferable beyond a specific speed, especially for long range AAMs.
Typical nonsense. The range of an AAM is related to the burn-time of a motor. Not a larger motor but a higher fuel-load will make the difference. 😎
Now that’s nitpicky enough to warrant a milder tone. Just assume he meant the propulsion unit in general. 😉
I’m writing from memory as it would take some time to find the relevant note book.
Something that comes up quite often. How about digitizing them?
Would keep them for posterity and would allow full text search. 🙂
By the way, is there a quantitative statistical law (something like Moore’s Law) that relates processing power to signal recognition?
I’ve been wondering about how modern computing advances influence IRST performance and would have liked to know whether there is some fairly constant growth to be expected.
You may be within the kinematic NEZ, but that’s academic if no firing solution is available.
I don’t remember it exactly, but I think the standard NEZ was fairly well defined, with something like “a target at 350kts doing a 6g turn and not being able to outrun the weapon” or similar.
You also have to look at the range that the launch platform can detect you, and the range at which the weapon can be employed effectively against you. There is a range at which weapons can be used against stealthy targets, where they have a low probability of escape, but you have to include the fire control/seeker limitations into the equation too.
Which is why being within the NEZ would be less risky for an LO/VLO type, but it’d still be within the kinematic NEZ.
Perhaps there is another term for a concept including the NEZ and the availability and range of target data or probability of target detection within NEZ?