Classified · Fighter Class · Interceptor Specification

FIRST CLASS GALACTIC — MILITARY DIVISIONSPECTER-1

LONG-RANGE HIGH-IMPACT INTERCEPTOR

Smaller. Faster. Deadlier than the Ovalion. One pilot. Scalar drive. Neural interface. Scalar pulse cannon. 0.04c maximum velocity. Designed to end an engagement before the enemy knows it has begun.

Specter-1 Interceptor — Low Earth Orbit

SPECTER-1 INTERCEPTOR · LOW EARTH ORBIT · FIRST CLASS GALACTIC MILITARY DIVISION

— Specter-1 · Three-View Engineering Schematic —

TOP VIEW — DORSAL PLAN

28.0 m18.0 mSEG RING · 1.8m ØCOCKPITDRIVES ×4NOSE / SENSORELF PODPULSE RAILSDELTA WING

SIDE VIEW — STARBOARD PROFILE

5.2 mSEG COREPILOTION DRIVESPULSE CANNONDORSAL FINELF POD

FRONT VIEW — BOW / NOSE-ON

18.0 m WINGSPANCOCKPITSEG COREPULSE ×2ELF PODION ×4

28 m

Length

0.04c

Max Velocity

2.4M km

Range

180 MW

Strike Power

ENGINEERING DRAWINGS — SPECTER-1

CONCEPT PHASE · DWG SET SP1-001/003

SP1-001 · PLAN VIEW (TOP ELEVATION)

28.0 m OVERALL LENGTH18.0 m SPANSEG RING · Ø1.8m · 340 MWeCOCKPIT · NEURAL I/F4× ION PODS · 360° GIMBALPULSE CANNON · 180 MWFIRST CLASS GALACTIC · MILITARY DIVSPECTER-1 INTERCEPTORPLAN VIEW — TOP ELEVATIONDWG: SP1-001 · SCALE 1:200 · REV A · CONCEPT

SP1-002 · SIDE ELEVATION (STARBOARD)

SEG28.0 m5.2 m HEIGHTNOSE / SENSOR ARRAYCANOPY · Au-COATEDSEG · 340 MWeFR01FR02FR03FR04FR05FIRST CLASS GALACTICSPECTER-1 SIDE ELEVDWG: SP1-002 · 1:200 · REV A · CONCEPT

SP1-003 · INTERNAL LAYOUT — MID CROSS SECTION

COCKPITNEURAL I/F · 270° DISPLAYSEGØ1.8m · 340 MWe · 7.83 HzSCALAR MISSILE BAY (×9)SCALAR MISSILE BAY (×9)LIFESUPP90 DAYXe TANK1,200 kgCAP BANK6 GJ · 4-sec chargeFIRST CLASS GALACTICSPECTER-1 CROSS-SECDWG: SP1-003 · 1:100 · REV A · CONCEPT

ALL DRAWINGS CONCEPT REFERENCE ONLY · FIRST CLASS GALACTIC · OPEN SOURCE · 2025

Physical Depiction & Internal Architecture

HULL FORM & GEOMETRY

Configuration

Cranked double-delta with swept variable-geometry outer panels

Fuselage Cross-Section

Flattened elliptical — 5.2 m tall × 6.8 m wide at widest point amidships

Nose Geometry

Ogival cone — 3.2 m length — houses phased scalar sensor array in tip fairing

Wing Sweep (inner delta)

72° leading-edge sweep — fixed — carries all primary hardpoints

Wing Sweep (outer panel)

35°–68° variable — extends fully for atmospheric cruise, retracts flush for orbital sprint

Dorsal Fin

Single swept ventral-dorsal stabiliser pair — 3.8 m height — integral ELF antenna embedded in skin

Chine Edges

Sharp leading chines from nose to engine intake — serve dual function: shock management + scalar field shaping

Hull Material (outer skin)

Titanium-graphene composite laminate — 12 mm primary skin — 98% EM transparency for scalar field projection

Hull Material (frame)

Osmium-carbon nanotube spaceframe — 40% lighter than equivalent titanium monocoque — hardened against ELF intrusion

Thermal Coating

Black-body scalar-absorptive ceramic outer layer — emissivity < 0.02 — invisible in IR at operating temperatures

INTERNAL ARCHITECTURE — CROSS-SECTION LAYOUT

Zone A (Nose, 0–3.2 m)

Scalar sensor array, forward phased array, IFF transponder, targeting computer node — all in pressurised avionics bay

Zone B (Forward fuselage, 3.2–10 m)

Dual pulse cannon mounting cradles — lateral feed from capacitor banks — 6 internal missile bays (3 per side)

Zone C (Cockpit, 8–12 m from nose)

Armoured titanium tub — 270° panoramic display shell — neural interface mount — biofield emitter ring at seat base

Zone D (Centre, 12–18 m)

SEG ring assembly — 1.8 m diameter, 0.9 m depth — vibration-isolated on 6-point mount — capacitor bank ring surrounding

Zone E (Mid aft, 18–23 m)

Fuel cell banks (xenon, 1,200 kg), life support module, autonomous AI core, crystal shield node × 8

Zone F (Engine bay, 23–28 m)

4 × vectored ion thruster gimbals — 360° pitch-yaw — scalar drive secondary field coils

Wing Roots

Integral structural spars carry hardpoint loads directly to spaceframe — no separate pylon attachment — zero shear risk

Belly Fairing

Landing gear bay (deployable strut system) + 4 × external hardpoint pylons recessed flush when retracted

SEG CORE — ENGINEERING DETAIL

Ring Diameter

1.8 m — smallest viable production SEG for full mass-reduction envelope

Rotor Configuration

3-ring neodymium-iron-boron array — inner, mid, outer — contra-rotating

Magnet Count

18 / 36 / 72 per ring — sized per Searl reciprocal-of-square law

Resonant Lock Frequency

7.83 Hz Schumann base — harmonic at 14.3, 20.8 Hz active during sprint mode

Output (nominal cruise)

140 MWe — sustains flight systems, shields, comms, and 60% weapons ready

Output (combat)

340 MWe — full weapons, maximum shield, full thrust simultaneously for up to 8 minutes

Output (sprint burst)

640 MWe peak — 8-second maximum — induces mass reduction to 1.8% effective — velocity spike

Thermal Management

Zero waste heat in vacuum — SEG output is direct electricity. Minimal IR signature inherent to design.

Isolation Mount

6-point ferromagnetic damped cradle — decoupled from hull vibration — field symmetry maintained to ±0.003%

COCKPIT & PILOT ERGONOMICS

Seat Type

Zero-G contour shell — custom-fitted per pilot — lateral support for 80g dampened (3g experienced)

Helmet Interface

Full-skull biofield headset — 128-channel EEG pickup — non-invasive — 0.08s thought latency

Display Surface

270° wrap — 12 × micro-display tiles — seamless — outer hull camera array feeds direct feed

Physical Controls

Side-stick + throttle quadrant retained as backup — used by trainees — most pilots set to standby after familiarisation

Biofield Ring

7.83 Hz scalar emitter ring embedded in seat base and overhead arch — maintains pilot coherence at combat stress levels

Ejection System

Full cockpit tub ejection — 0.04 second separation — capsule has 72-hour independent life support + return beacon

Suit Integration

Pilot suit hardwired to cockpit biometrics — HRV, SpO2, cortisol, temperature — AI monitors degradation and escalates to autonomous mode

Cockpit Dimensions

1.8 m wide × 2.1 m long × 1.4 m seated headroom — pressurised to 0.85 atm during deep space ops

Systems Engineering Specifications

Class

Specter-1 Interceptor

Single-pilot long-range high-impact strike vessel

Role

Fighter / Interceptor / Deep Strike

Anti-vessel, anti-satellite, precision planetary strike

Length

28 m

Versus Ovalion 180 m — purpose-built for speed and agility

Width (wing span)

18 m

Variable geometry wings — deploy for atmospheric, retract for orbital

Height

5.2 m

Low-profile fuselage — minimises radar and scalar cross-section

Mass (combat ready)

42 tonnes

Stripped for speed — no crew quarters, no cargo

Crew

1 pilot / optional 1 weapons officer

Single-seat primary config — tandem cockpit variant available

Hull Material

Titanium-graphene monocoque

Same Station Alpha material — 60% lighter than steel equivalent

Scalar Signature

Class-1 Stealth — 98% field suppression

Scalar dampener coil reduces EM and etheric detection to near-zero

Operational Range

2.4 million km unrefuelled

Earth to Moon and back × 6 — or sustained LEO patrol for 90 days

ENGINEERING NOTES

The Specter-1 is the blade where the Ovalion is the warship. Designed around a single principle: get there fast, hit hard, vanish. Every gram of mass is justified — no redundancy that does not serve lethality or survival. The vessel is optimised for the pilot — biofield-integrated cockpit, Schumann-locked neural interface, and a SEG core dimensioned precisely to the mission envelope.

SPECTER-1 vs OVALION — COMPARISON

ATTRIBUTE

Length

Mass

Power Output

Crew

Role

Max Speed

SPECTER-1

28 m

42 t

340 MWe

1–2

Fighter / Strike

0.04c

OVALION

180 m

8,400 t

12 GWe

120

Warship / Carrier

0.01c

— SERGEANT'S FIELD NOTE —

"The Specter-1 is not a weapons platform. It is an argument-ender. One vessel. One pilot. One scalar pulse. The purpose is not destruction — it is absolute deterrence. When the adversary knows this vessel exists and what it can do, the argument never starts."