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
| Stowed — bar flush on forward sleeve | Deployed — shoulder bar at 12→6 (vertical) |
|---|---|
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Thin ~6 in fold-down bar on the forward black sleeve; visible hinge; no fixed shoulder stock. Full geometry: shoulder bar spec.
Tank-shell tube (stays in launcher; rocket flies free) · Pop top → load → unscrew bottom in bore → close → rocket ready. Art: side left = top, right = breech. Spec: CONTAINER-SPEC.
18 in self-contained round inside the tube; fins stowed for clearance. Left = nose (seeker), right = tail (nozzle). Spec: ROUND-SPEC.
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 Bazooka — 40 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.
| 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.
| 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 N → 1050–1150 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 |
| 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.
| 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 |
- Open breech — pull spring-loaded bolt handle and swing breech open
- Pop top (PULL tab) on alloy tube
- Slide tube into launcher bore until seated
- Unscrew bottom screw cap in bore (gloves OK)
- Close breech — deadbolt snap → rocket ready (electrical continuity)
- Hold front trigger — seeker + lock tone; retention stop disengages
- Pull rear trigger (front held) → rocket flies free (recoilless vent ≤ 10 yd rear)
- 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
| 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
Laser beam-riding · Launcher-tracked guidance · Kinetic penetrator rod · High off-boresight agility · General-issue every-rifleman distribution
| 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
| 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 |
| Doc | Purpose |
|---|---|
| One-pager | Single-page concept summary |
| Pitch deck outline | 8–10 slide structure |
| Licensing & partnership | Prime teaming, IP tiers, inquiry path |
- 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)
| 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.



