The VAK-191 looks like some weird hybrid of Harrier and Forger... with all their flaws and no advantage.
"hey let's build a Harrier with a Pegasus look alike but much smaller engine with a smaller compressor so that it can get supersonic"
"Good idea, alas the engine is not powerful enough for VTOL"
"Well then let's steal the Forger two lift jets and voilà, problem solved"
"Yeah but one behind the cockpit, as in the Forger, but the other one in the tail. This is more balanced."
Hot gas re-ingestion issues must have been pretty fun, with one lift-jet fore, another aft, plus two rotating exhausts also on the rear.
The Forger is certainly much maligned for good reasons, but the VAK-191B... the Germans were wise to abandon that one.
Had they dropped the lift jets, they would have had a supersonic-but-non-VTOL (STOL only) Harrier little brother.
Hello,
counter: "The Forger looks like some weird hybrid of a Yak36, VAK191 and Harrier?
The use of lift engines might have been a good decision.
If you do not need a more powerfull engine for forward flight, because the design goal is subsonic, 250 kg for 2 lift engines might be less than the additional weight of a bigger "Pegasus" and the higher fuel comsumption during the whole flight compared to some fuel for lift engines during VTOL-time for a minute or two.
Hot gas re-ingestion is no fun for EVERY VTOL-plane.
The VAK could easily be topped by the Do 31 with 2 Pegasus and 8 (!) additional ift engines.
That's why they "developed" forward moving VTOL-take-off and landing or the jump-start.
It also does not ruin the surface of the runway that fast.
The VJ101 for example has 4 afterburners "hitting" the runway. Even a stainless steel runway wouldn't have taken that without damage.
The thrust of the RB193 would have been developed during time, like the Pegasus too (from 49kN to 106 kN !).
So, most of these VTOL-planes have been designed with the knowledge of that time for some different tasks in mind.
The technical solutions were very interesting. Most of them "died" due to changes in military requests and not by not-fulfilling the design goals.
Uli