[NEWS]Seed round closed - Isengard in Y Combinator - Summer 2026UNCLASSIFIED // PUBLIC RELEASE
// PROPULSION

Gas turbine systems

Propulsion.

Isengard TJ-100 turbojet engine

Overview

Power, built in-house.

Propulsion is the bottleneck most strike systems never solve. Isengard designs and builds its own turbojets - combat-tested, rate-producible, and tuned for the airframes they fly. Two engines anchor the line - the cruise-missile-class TJ-100 and the compact TJ-40 - with the 200 kgf class TJ200 now in validation.

TJ-100 turbojet, side profile

TJ-100 turbojet

Cruise-missile class.

A combat-tested single-spool turbojet for high-subsonic strike systems - qualified, fielded, and ready for rate production. Two TJ-100s power the XQ 770 Freedom Fighter.

1,000 N
Thrust class
TRL 9
Maturity
TJ-100 datasheet
Engine typeSingle-spool turbojetJet A-1
Thrust class1,000 N~225 lbf
MaturityTRL 9Combat-tested
ApplicationXQ 770 (x2)High-subsonic strike
TJ-40 turbine, side profile

TJ-40 turbine

Compact class 40.

A single-spool turbojet for unmanned aerial vehicles and defense platforms - a balance of thrust, efficiency, and rugged reliability in a tightly packaged, airframe-ready envelope.

40 kgf
Max thrust
10.8:1
Thrust / weight
TJ-40 datasheet
Max thrust @ 100% RPM392 N / 40 kgf88.2 lbf
Dry weight3.7 kg8.16 lb
Max rotational speed98,000 rpmidle 40,800 rpm
Compressor pressure ratio3.8 : 1single-spool
Thrust-to-weight10.8 : 1dry
Outer diameter148 mm5.83 in
Overall length370 mm14.57 in
Recommended fuelJet A-1 / Kerosene1.2 lpm
TJ200 turbojet, side profile rendering

TJ200 turbojet · in validation

Class 200.

A 200 kgf class single-spool turbojet - intake, compressor, annular combustor, turbine and nozzle under the Warden FADEC. The baseline is dry; an optional afterburning section is selected by mission requirement and rated separately. Values are the current design specification.

200 kgf
Max thrust, dry
30 kg
Dry weight
TJ200 technical data
Thrust, dry200 kgf441 lbf
Governed speed41,500 rpmmargin 42,000 rpm
TSFC at rating1.38 kg/kgf·h4.60 kg/min
EGT, max850 °C1,562 °F
Diameter · length32 · 72 cm12.6 · 28.3 in
Dry weight30 kg66 lb
Max Mach0.95−40 to +50 °C ambient
ControlWarden FADECCAN · RS-485 · analog
StartingElectric · 70 sto 4,500 m
ConfigurationDry baselineafterburner option

Design curves, to be replaced with calibrated test-cell data after validation. Controlled release: final specification, operating limits and certification values issue after the TJ200 validation cycle.

Why in-house

Engineered for the airframe.

Packaging

Compact & light

Tightly packaged envelopes for straightforward UAV integration across the strike line.

Response

Rapid throttle

Fast spool dynamics for responsive tactical control, with a fuel-efficient cycle that extends endurance.

Production

Rugged & rate-ready

Built for mass production and field reliability - customizable nozzle and mounting options per platform.

Isengard gas turbine systems

Request the propulsion datasheets.

Full TJ-100, TJ-40 and TJ200 performance and integration data are available to allied governments, primes, and qualified partners.

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