Two very interesting comments- Su-37 “Super Terminator” and “Ultra Terminator”

Hi everyone!

There have not been very many posts recently, I aim to do more in the future, but it is difficult to find time! I will soon bring out a post on NATO codenames.

But now I will show you two very interesting comments by dr. nick stage–PHD which he put onto my old blog (I used to have a different blog, but then I started this one which is better).

Here are the comments by dr. nick stage–PHD :

Comment 1:

“The new Russian Sukhoi SU-37 jet fighter aircraft
can be modified into a new SU-37 ULTRA-SUPER
FLANKER Jet.

There would be a 2-man crew–PILOT, and sitting in tandem with the Navigator-Weapons REO Officer.

A new engine, a modified Llukya AL-41,
would weigh–with after-burner, 2,950 Lbs.,
and in non-after-burner mode generate
27,700 lbs. of thrust–a thrust to weight
ratio of 9.4-to-1.0.
In after-burner operations, the maximum
thrust of 46,350 lbs. of thrust–a 16.6
to-1.00 the thrust to weight ratio.

Combat Radius—–970 miles–2-engined versions.
Combat Radius—–786 miles–3-engine versions.

Climb Rate—79,500 feet per minute-2 jet engines.
Climb Rate—94,200 feet per minute-3 jet engines.

Service ceiling altitude–70,480 feet.

A compression Ratio of 33.8-1.00; comparable
to the new USAF F-22 “Raptor” jet engine 35.10
to 1.00 compression Ratio.

Aircraft base weight————29,600 lbs.
Fully loaded aircraft weight—-61,000 lbs.

both above–2 new jet engines.

Total aircraft weight-to-thrust ratio
of 1.00-to-1.52.
——————————

With the 3-engined version——–38,230 lbs.,
base weight, and 72,000 lbs, fully-loaded.
Total aircraft weight to thrust ratio of
1.00-to-2.44.

All 2-engined versions would have 2 jet
engines with vectored-exhaust thrust nozzles.

In the 3-engined version, the center-engine
would be used to keep the aircraft steadied.
This center engine would not have vectored thrust,
but it’s maximum thrust, in after-burner mode
would be 61,650lbs. of thrust—–essentially
a turbo-rocket RAM JET, for a “max-thrust”
for periods of up to 225 seconds–in Methane Gas
Injection!
To elaborate further:
There would Methane Gas Injection into
a tapered exhaust-section, giving this jet
a “kick-boot” in climbing.

In terms of G-loads—–maximum in turns–14.2 Gs.
In flight, a negative 4.5 Gs and up to a positive
12.5 Gs.

———————————–

On-board armaments:

1—-44 MILLIMETER CANNON–Nose of aircraft
with 109 rounds—3 per second of cyclic rate of fire. Each of the cannon shell would have a fusing
proximity-control to cause rounds to explode
in a shower of fragments 20-to-30 meters from
enemy target jet.
Shell velocity —4,400 feet per second.

2—-60-caliber wing machine guns—490 rounds
each, with a cyclic firing rate of 1,050 rounds
per minute–or 18.4 rounds per second.
Each round would have depleted-coated “slug”.

4-to-6 “Super-Phoenix”-type air-to-air missiles
with an effective 240-kilometer range, at
MACH 5.65. These missiles would be anti-satellite
ASAT-capable, also, especially during a modified
“Pugachev Cobra” manuever.
ALSO;
These missiles will carried internally
like in the USAF F-22 “Raptor” jets air-to-air
missiles.

On the wing “hard-points”, 4 “Super Sidewinder”
air-to-air missile—13.6 kilometer range
and at MACH 3.5 ,in speed.
Hard-points with missiles would have
a 11.8 G maximum turning force, before this G-force
would tear-off the missiles in a turn.

On board-avionics will be able to track
up to 10 targets, at the same time.

———————————————–

Instead of a long runway for take-off,
the mode of launching this aircraft would
be railed-sleds that are 580 meters in length.
This will be a 60-degree up-angle of launching
sled system.

The aircraft would have 4-to-8 JATO-RATO
launch-boosters, each generating 8,700 lbs of thrust for 22-to-31 seconds.
These rocket JATO-RATO boosters would be
jettisoned 3 seconds before aircraft lifts-off
from the launch-sled. G-Load–7.7-to-9.0Gs.

Just before launching this aircraft on the rail-
sleds, by 10 seconds before JATO-RATO ignition,
the aircraft will be in FULL-POWER-THROTTLE
Mode. At Lift-Off, the middle or core engine
will have a 35 second injection of Liquid
Methane into both the Combustor stages, but also
a 45 second Liquid Methane injection the
after-burner section, for a added “kick-boost”.

During this time, the two outer engines
will be at “full throttle”, at a vectored-exhaust
upward angle of 50 degrees for 24 seconds, then
back to horizontal-mode.

==============================================

This is my proposal for this ULTRA-SUPER-
FLANKER—call it the Sukhoi SU-37MMM-k-3,
or the “Super-Terminator” for the twin-engined
version, and the “Ultra-Terminator” ,for the
3-engined version.

Thank You:

from Dr. Nick Stage–PHD.
Indiana.”

Comment 2:

“As a back-up:

This proposed Ultra-Flanker-Ultra Terminator
Sukhoi Jet, would be MACH-2.0-capable at Sea Level,
a cruising speed at a maximum of MACH 2.75-plus,
and a maximum speed in the 2-engined version
of MACH 3.10, and in the 3-engined version
a MAXIMUM SPEED–for up to 395-430 seconds of
MACH 3.50-plus.

Thanks Again:
from
Dr. Nick Stage-PHD.
Indiana. ”

Thanks for the comments!

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One Response

  1. That is one of the best jets ever made!

    Download FSInn FSCopilot

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