Skip to content

Fratres-X-AI/RADR-mk.60

Repository files navigation

RADR — Recoilless Anti-Drone Rocket

Squad / SOF Mid-Range Drone Destroyer — 60 mm Class

RADR is a lightweight, reusable 60 mm shoulder-fired recoilless rocket system for squad and SOF — a mid-range drone destroyer that emphasizes speed-to-target, simplicity (KISS), reliability, and one-person reload. It engages Group 1–2 threats (FPV, quadcopters, loitering munitions, terrain-matching/gliding drones) as a mid-range counter-UAS weapon when machine guns fall short and SAM is too heavy to allocate.

Status: Phase 0 — Conceptual
Version: 1.8.2

Launcher concept art

Stowed — bar flush on forward sleeve Deployed — shoulder bar at 12→6 (vertical)
RADR launcher — shoulder bar stowed RADR launcher — shoulder bar deployed

Thin ~6 in fold-down bar on the forward black sleeve; visible hinge; no fixed shoulder stock. Full geometry: shoulder bar spec.

Round container (alloy tube)

RADR alloy protective tube — pop top, screw bottom

Tank-shell tube (stays in launcher; rocket flies free) · Pop toploadunscrew bottom in bore → close → rocket ready. Art: side left = top, right = breech. Spec: CONTAINER-SPEC.

Round (18 in rocket)

RADR mk.60 round — stowed fins, authoritative

18 in self-contained round inside the tube; fins stowed for clearance. Left = nose (seeker), right = tail (nozzle). Spec: ROUND-SPEC.


Core Vision

The gunner rough-aims on a fold-out display fed by an integrated digital camera-style sight (smooth 1×–20× zoom via foregrip + / −). RPG-style shouldering — arm’s-length view on the panel; no cheek weld or perfect sight picture required. Holding the front trigger powers the round’s 100 mm IR fire-and-forget seeker and yields a steady lock tone; the rocket retention stop disengages only then. Pulling the rear trigger (while holding front) launches the 18-inch round from an alloy protective tube. A mildly progressive solid motor drives closure to ~330–350 m/s at 1000 m. Moderate-maneuver nose canards trim the flight path; four swept spring-loaded fins deploy at exit and mechanically lock open. At ~20 ft, radar or millimeter-wave proximity (with timed backup) fires a pyrotechnic dispersal charge that throws 300 × 7 mm rough-edged dense alloy cubes in a forward-biased cone (~10–12 ft wide). The cubes kill — not a kinetic rod.

Philosophy: Speed is the primary defense · KISS + rugged · One-person reload · Honest capability ceiling.

Launcher: Modernized M1 Bazooka40 in tube (≤ 5.5 kg empty), matte camo, Gustav-style flip breech (spring bolt + positive deadbolt lock), dual pistol-style triggers (rear grip just aft of sight module; front slightly smaller; + / − zoom on foregrip aft face, wired to sight + display), 6 in fold-down shoulder bar (slim rounded pad, stows flush on barrel; deploys 12→6 vertical — no add-on end cap), no fixed shoulder stock, slightly rear-biased balance.


Primary Threats

Threat class Examples / notes
FPV kamikaze drones Close-in attack profiles; high closure rate
Small-to-medium quadcopters ISR, spotter, and light attack platforms
Loitering munitions Orbiting or diving engagement profiles
Terrain-matching / GPS-denied gliders Low-signature glide profiles (e.g. Hornet / “Martian” class)
Group 1–2 UAS (general) Swarm and interdiction attacks in the close fight

RADR is not sized for large Group 3+ platforms or long-range aircraft.


Locked Specifications

Item Spec Status
Role Mid-range drone destroyer; squad / SOF mid-range counter-UAS Locked
Caliber 60 mm Locked
Rocket length 18 in (457 mm) maximum Locked
Launcher length 40 in (1016 mm) Locked
Rocket mass (target) ≤ 3.5 kg Locked
Launcher empty mass (target) ≤ 5.5 kg Locked
Warhead 300 × 7 mm dense alloy rough-edged cubes Locked
Dispersal Pyrotechnic dispersal charge — forward-biased cone ~10–12 ft wide @ ~20 ft Locked
Fuze Radar or mm-wave proximity (primary) + timed backup Locked
Seeker 100 mm IR fire-and-forget Locked
Guidance Moderate-maneuver; small movable canards near nose Locked
Fins 4 swept spring-loaded at base; deploy on exit; mechanical lock once deployed Locked
Motor Mildly progressive solid; 2950–3050 N·s; ~3.3 s; 750–850 N1050–1150 N peak; ~330–350 m/s @ 1000 m Locked
Range 200 m min · 800–1200 m band · 1000 m sweet spot · 1200 m max; 330–350 m/s @ 1000 m Locked
Backblast ≤ 10 yards (30 ft) Locked
Protective tube Tank-shell alloy/composite tube — PULL pop top; screw bottom in bore; foil contacts → rocket ready Locked
Breech Gustav-style flip; spring-loaded bolt + positive mechanical lock (bolt-action feel) Locked
Controls Front = seeker + audible tone; rear = fire (front held) Locked
Shoulder bar 6 in thin rod; hinge on forward black sleeve; stowed / deployed Locked
CoG Slightly rear-biased (comfortable shouldering) Locked
Rocket retention stop Bore stop when slung; releases only: breech closed + front held + lock tone Locked
Sight / power Integrated digital cam sight; smooth 1×–20× zoom (+ / − on foregrip); fold-out ~4 in display; grip battery Locked

Validated vs notional (summary)

Item Status
300 cubes, range envelope, employment, authoritative art Locked requirement
v@1000, CdA, mass/CG fragment check Modeled + CI
MC 25k @ 1000 m (99.76% in 330–350 m/s) Statistical
Motor, seeker, fuze, lethality (Pk) Notional / untested
275-cube @ 1200 m Archived trade-study

Full matrix: Annex I — Validated vs notional traceability.


Safety (Layers)

Layer Function
Rocket retention stop Mechanical stop in barrel prevents round sliding forward when slung or carried; disengages only when breech is fully closed, gunner holds front trigger, and seeker outputs steady lock tone; re-engages if front is released
Breech deadbolt Positive mechanical lock when closed — no seeker or retention release until tube seated
Dual-trigger interlock Rear fire blocked until lock tone; front must stay held through ignition
No override No rear fire without tone; no seeker until tube seated
Backblast discipline 10 yd (30 ft) cleared to rear before every shot and before breech re-open

Operational Sequence (Locked)

  1. Open breech — pull spring-loaded bolt handle and swing breech open
  2. Pop top (PULL tab) on alloy tube
  3. Slide tube into launcher bore until seated
  4. Unscrew bottom screw cap in bore (gloves OK)
  5. Close breech — deadbolt snap → rocket ready (electrical continuity)
  6. Hold front trigger — seeker + lock tone; retention stop disengages
  7. Pull rear trigger (front held) → rocket flies free (recoilless vent ≤ 10 yd rear)
  8. Open breech — spent protective tube drops out for reload

Carry: Launcher + one round ≤ 9.0 kg — one person can reload. Retention stop engaged whenever front trigger is not held.

Authoritative detail: Annex F — Gunner sequence · Breech · Retention stop · DOC-06 diagrams


Comparison Snapshot

RADR Carl Gustaf M4 FIM-92 Stinger
Role Mid-range C-UAS Multi-role MANPADS
Launcher ≤ 5.5 kg, 40 in ~6.6 kg ~15 kg
Round ≤ 3.5 kg, 18 in ~3.2 kg ~10.1 kg
Guidance IR F&F, moderate-maneuver Unguided High-agility IR
Range goal 1000 m ammo-dependent 4000+ m
Backblast 10 yd (30 ft) ~60 m class moderate

Data: data/baseline_systems.json


Out of Scope (Removed Concepts)

Laser beam-riding · Launcher-tracked guidance · Kinetic penetrator rod · High off-boresight agility · General-issue every-rifleman distribution


Engineering models (notional)

Tool Purpose
scripts/radr_performance_model.py 2-D ballistics v2 — (C_d A) in m², ranges 200–1200 m, CI --verify
data/performance_model_output.json Regenerated tables (TOF, Mach, (q), sensitivity, evasion)
scripts/mass_cg_calc.py Mass/CG + 300×7 mm fragment mass check
scripts/guidance_evasion_sanity.py Moderate-maneuver vs lateral evasion (geometric sanity)
notebooks/RADR_Performance_Dashboard.ipynb Jupyter pitch dashboard (RunPod or local)
pip install -r requirements-modeling.txt
python scripts/radr_performance_model.py --verify
jupyter lab notebooks/

RunPod: notebooks/RUNPOD-QUICKSTART.md./scripts/runpod_max_cpu.sh uses 32 workers (4090 = Jupyter; math is CPU).

Detail: Annex I — Performance Modeling


Document Map

# Document
01 Concept Overview
02 Operational Requirements
03 Design Constraints
04 CONOPS / Use Cases
05 Key Design Trades
06 System Description
07 Limitations and Risks
08 Layered Defense Integration
09 Motor Vendor Brief
10 Phase 1 Prototype Gates
11 Live-fire & Partner Validation
Annex Topic
A–E Baseline, KPPs, trades, stabilization, references
F Employment sequence & breech
G Mass budget & CG
H Motor thrust curve
I Performance modeling
J Warhead dispersal

Outreach

Doc Purpose
One-pager Single-page concept summary
Pitch deck outline 8–10 slide structure
Licensing & partnership Prime teaming, IP tiers, inquiry path

Open Questions

  • Live-fire Pk at 1000 m by threat class (hover vs. crossing vs. glide)
  • Evolution Space grain geometry vs. measured backblast inside 10 yd zone (motor baseline locked; live-fire TBD)
  • Cube alloy finalization (dense Ti/steel baseline)
  • Retention stop mechanism detail (spring/cam vs. solenoid assist) — function locked
  • Fuze baseline down-select: radar proximity vs. millimeter-wave proximity (one primary per round)

License & prime partnership

Tier Document
Open concept LICENSE — MIT (docs, JSON, art)
Prime / Program LICENSE-COMMERCIAL.md — development & production under PCA

Teaming with a prime? Start here: Licensing & partnership · Partnership inquiry

All specs and art are notional; not authorization to procure, manufacture, export, or field any weapon system.

About

RADR — Recoilless Anti-Drone Rocket. Phase 0 concept: 40in 60mm squad/SOF terminal counter-UAS launcher + guided flak rocket.

Topics

Resources

License

Unknown, Unknown licenses found

Licenses found

Unknown
LICENSE
Unknown
LICENSE-COMMERCIAL.md

Contributing

Stars

Watchers

Forks

Releases

No releases published

Packages

 
 
 

Contributors