In article ,
"John Carrier" writes:
Did the Zipper C model get the higher output J-79? I'm sure the A was
lighter and cleaner. Any less stable w/o the ventral fin? The F-8 ventrals
were installed to improve supersonic stability, the A's and B's were a
little squirrely in the 1.5 range or so. Even the C/K would do a slow dutch
roll @ high mach if the yaw stab was not up to spec.

R / John

R / John
"WaltBJ" wrote in message
om...
Bunch of kids. 22 Jan 1931, Ketchikan, Alaska. USAF Aviation Cadet
Class 54-H, 28 Apr 54. F86F Sabrejet, F86Dog, F102, F104A, F4, 2000+.
Last flight in F4 Jan 31 80. Hung it up for good 31 March 80. Carter
wore me out. 104A with the J79-19 engine - yahoo! .9 to 2.0. 27 miles.
1'45", 1000 pounds of fuel....
Walt BJ



Walt flew the Hot Rod Model A's - an early air-to-air only F-104A with
the original small-0bore -3 engine replaced with the -19 engine used
on teh F-4E. They literally had about a Metric Ton more push than the
C model (I know, I know, I'm mixing units here, but I'm waxing
hyperbolic here), and performance that the documents I have on it,
and computations I've done have to be seen to be believed.
According to my quick reference (F-104A (-10 Engine) SAC Chart, June
1970)
The upper right corner of teh envelope is Mach 2+/67,000'. The whole
envelope ios bordered by either Q or airfrae heat limits - it never
runs out of power. During a Point Intercept mission,it would be
passing 30Kft in less than a minute after breaking ground.
(Oh, yeah - since it could fly so high, it would go just as far at
Mach 2 as it would a Mach 0.9)
I'm in awe of the beast.

--
Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster