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ALT: 3,200 FT
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    Aircraft Arresting Gear (AAG) System / Net-Based Runway Arresting Barrier / Dual 20T+40T Water-Twister Absorber / India
    RUNWAY SAFETY · EMERGENCY ARRESTING SYSTEM

    Aircraft Arresting Gear (AAG) System — stops 6,000–40,000 kg aircraft within 270 m at 3g.

    A permanent, net-based emergency runway arresting barrier for fighter and tactical aircraft. Twin stanchion towers raise a high-strength Nylon-66 net across the runway over-run; on engagement, textile purchase tapes drive a dual 20T + 40T water-twister energy absorber, converting kinetic energy into fluid-shear heat and bringing the aircraft to a controlled stop — reset in 10–15 minutes.

    Aircraft Arresting Gear system — labeled rendering showing the stanchion system and stacked energy absorber system with cable-guide wheels
    Fig · 01 Labeled system rendering — stanchion & stacked energy-absorber assemblies (not a photograph)
    Aircraft Mass Range
    6–40tonnes
    Max Deceleration
    ≈3g, controlled
    Max Run-Out
    270m
    Energy Absorber
    20T+40Twater-twister
    Reset Time
    10–15minutes
    Nylon-66 net · MIL-B-83183B tape handling Sheave housings to IS 9975-1981 Stanchions in IS 2062 E250 structural steel Engineered to order Noida · India
    01
    Overview

    The last engineered safeguard at the runway end.

    When brakes, runway length and pilot margins are all exhausted, the AAG converts an uncontrolled overshoot into a predictable engineering event.

    Aircraft Arresting Gear system design drawing — general arrangement of the runway arresting installation
    Fig · 02 Design drawing — general arrangement (not a photograph)

    The Aircraft Arresting Gear (AAG) System is installed as a permanent, always-ready safety barrier aligned with the runway over-run at each end. It uses a high-strength Nylon-66 net, textile purchase tapes and a dual 20T + 40T water-twister energy absorber to safely stop aircraft in the 6,000–40,000 kg class within a controlled run-out of up to approximately 270 m, holding peak deceleration to around 3g so the aircraft and pilot can walk away from an otherwise catastrophic overrun.

    It is not a comfort feature — it is engineered for the worst single day in the life of a runway: a rejected take-off at high gross weight, a landing overrun on a wet or contaminated surface, a brake or hydraulic failure, or a crosswind touchdown that shifts the stopping point unfavourably. In every one of these scenarios, the AAG provides a repeatable, measurable, engineered stop rather than a random excursion beyond the runway end.

    When everything goes wrong, the AAG is the only thing that still has to work — first time, every time.
    02
    Architecture

    Seven subsystems, one arresting event.

    Each runway end carries a defined set of mechanical, electrical and civil subsystems that together deliver the arresting function.

    Sub · 01

    Multi-Element Net Assembly (MENA)

    High-tenacity Nylon-66 net, approximately 58 m wide and 4.7-4.9 m high, built from 40 vertical elements (>3,400 kgf) interconnected by horizontal straps (>2,300 kgf), wrapping around the nose, fuselage and wing root on engagement.

    Sub · 02

    Net Anchors (NA) & Engagement Support System (ESS)

    17 net anchors across the arresting lane, released via a 2,500 kgf shear pin; 11 mm suspension rope and 8 mm restraining ropes, with a 44 kN load cell for tension monitoring.

    Sub · 03

    Stanchion Systems (STS)

    Two hinged steel towers per runway end, approximately 7.5 m tall in IS 2062 E250 structural steel, raising the net to full height in about 3 seconds via a ~19 HP geared motor with brake.

    Sub · 04

    Tape Connector (TC) & Purchase Tape (PT)

    Alloy-steel tape connector with a balanced strain-gauge load cell and DAQ, linked to high-strength textile purchase tape that transmits load from the net to the energy absorber.

    Sub · 05

    Energy Absorber Assembly (EAA)

    Dual stacked water-twister units rated 20T and 40T on a common frame, with a water plus ethylene-glycol working fluid and linear-actuator stage switching in under 5 seconds.

    Sub · 06

    Tape Retrieval, Pressure Roller & Sheave Assemblies

    Worm-gearbox tape retrieval system for 10-15 minute reset; pressure roller assembly meeting MIL-B-83183B tape-handling criteria; sheave housings built to IS 9975-1981.

    Sub · 07

    Electrical Control System, Control Hut & Civil Works

    ECS with full interlocks and alarms; control hut approximately 12 x 8 x 3.5 m with ~6 kW rooftop solar and DG provision; dedicated RCC foundations for every subsystem sized for dynamic arrest loads.

    03
    Design Drawing

    Design documentation.

    General arrangement drawing for the AAG system installation, available as PDF for procurement and technical review.

    04
    Specifications

    High-level technical data.

    Key parameters of the standard Neometrix Aircraft Arresting Gear System.

    Aircraft Mass RangeApproximately 6,000 kg to 40,000 kg
    Max Aircraft Deceleration≈ 3g, controlled, non-shock arrest
    Max Arresting Run-OutUp to 270 m, depending on entry speed and mass
    Arresting PrincipleNet capture + textile purchase tape + dual water-twister energy absorber
    Net (MENA) Width / Height≈ 58 m span · 4.7-4.9 m deployed height
    Net Vertical Elements40 high-tenacity Nylon-66 elements; vertical > 3,400 kgf, horizontal > 2,300 kgf
    Stanchion System2 per runway end, ≈ 7.5 m steel lattice frame, ~19 HP geared motor, net raise ≈ 3 s
    Energy AbsorberDual stacked water-twister (20T + 40T), water + ethylene-glycol working fluid
    Stage SwitchingLinear actuator, slider fork, < 5 s response
    Tape Retrieval / Reset10-15 minute full reset time
    Control Hut≈ 12 m x 8 m x 3.5 m; ECS with interlocks and alarms; ≈ 6 kW rooftop solar + DG provision
    Civil FoundationsDedicated RCC foundations for each subsystem, designed for dynamic arrest loads
    05
    Applications

    Where it is deployed.

    The AAG system serves as the last-resort safety barrier at fighter and naval aviation airbases.

    A · 01Emergency arrestment during brake failure, hydraulic failure, tyre burst or landing gear malfunction
    A · 02Routine operational arrestment of high-performance fighters and advanced trainers
    A · 03Safe aircraft recovery on short, restricted or geographically constrained runways
    A · 04Over-run protection on wet runway operations or landing miscalculations
    A · 05Training and qualification arrestments for pilots, technicians and emergency response teams
    A · 06Arrestment support for UAVs / UCAVs requiring controlled net-based capture
    A · 07Aircraft braking system evaluation and validation during flight trials
    A · 08Runway safety enhancement at military airbases and naval aviation facilities
    06
    In Depth

    From overshoot to controlled stop.

    Engineering narrative for programme managers and airfield safety teams evaluating the AAG system.

    Introduction

    On a modern fighter base, everything is designed around speed: high approach velocities, short decision windows, heavy weapon loads and tight sortie cycles. The same parameters that make a fighter effective in combat also make it unforgiving during an abnormal landing or aborted take-off. A fighter touching down long and fast on a wet runway, with anti-skid and brakes working but not enough friction or distance left, has soft ground, perimeter fencing, roads or populated areas beyond the runway lights. At that point, the base either has a dedicated, engineered emergency arresting system, or it is gambling a multi-million-dollar aircraft, a pilot's life and runway availability on luck.

    The Aircraft Arresting Gear (AAG) System is that engineered safeguard. Installed at each end of the runway, it uses a high-strength Nylon-66 net, textile purchase tapes and a dual 20T + 40T water-twister energy absorber to safely stop aircraft in the 6,000-40,000 kg class within a controlled run-out up to approximately 270 m, holding peak deceleration to around 3g so the aircraft and pilot can walk away from an otherwise catastrophic overrun.

    Arresting Concept — From Overshoot to Controlled Stop

    At its core, the AAG converts kinetic energy into heat in a water-glycol absorber, using the net and purchase tapes as the mechanical link. In an emergency, command is given and the two stanchion towers at the runway edges rapidly raise a wide textile net across the over-run. The aircraft enters and is enveloped by this net, which breaks calibrated shear pins and releases from its ground anchors. The net is connected to high-strength purchase tapes that run through sheaves and fairlead tubes to a dual water-twister energy absorber buried at the side of the runway. As the aircraft pulls the net and tapes forward, the absorber spins in a controlled water-glycol bath, converting kinetic energy into heat with a smoothly increasing torque, bringing the aircraft to a controlled stop within the design run-out. The tapes are then rewound, the net is re-rigged, and the system returns to standby.

    • Standby mode: net lowered and attached to net anchors; purchase tapes fully wound on the absorber drum; ECS monitoring all subsystem health.
    • Emergency deploy: controller triggers deployment from the control hut; stanchion systems raise the net to full arresting height in approximately 3 seconds.
    • Engagement: aircraft enters and wraps the net; load rises until ESS shear pins (≈ 2,500 kgf) fail and the net bottom releases, routing load into the purchase tapes.
    • Energy transfer & absorption: purchase tapes pay out through sheave assemblies and fairleads, driving the drum on the dual 20T+40T water-twister absorber; the ECS selects 20T, 40T or combined mode via a linear actuator (switching < 5 s).
    • Stop and reset: aircraft stops within the design run-out; the tape retrieval system rewinds the tapes, the net is lowered, inspected and re-secured — total turnaround typically 10-15 minutes.

    Safety, Maintainability & Operational Advantages

    The AAG provides a dedicated, engineered stop for the worst failure cases, not just an incremental improvement in normal operations. Load cells in the tape connector and ESS, along with rpm sensors on the sheaves, give quantifiable data for every arrest event, allowing validation of energy absorption and continuous improvement of procedures. A 10-15 minute reset time keeps the runway and squadron sortie rate intact after an arrest, and materials, seals, coatings and civil design are suited for temperature extremes, humidity, dust, heavy rain and salt-fog conditions common to airbases.

    Subsystems are modular — stanchions, absorbers, tape retrieval system, ESS, sheave assemblies, pressure roller assembly — enabling targeted maintenance without full system downtime, and the use of standard industrial components (bearings, gearboxes, motors) simplifies spares management. Scheduled inspections focus on net and purchase-tape condition, wire ropes, sheaves, bearings and seals, energy-absorber fluid health, and civil foundations and anchor points.

    Conclusion

    The Aircraft Arresting Gear (AAG) System is not a generic ground-support add-on — it is a mission-critical safety asset that stands between a high-speed overrun and a catastrophic loss of aircraft, runway and life. By combining a high-strength textile net, intelligently controlled purchase-tape handling, a dual-stage water-twister energy absorber and a robust control and foundation architecture, the system converts an uncontrolled emergency into a managed, instrumented, repeatable engineering event.

    07
    FAQ

    Common questions.

    Plain-language answers from the engineering team.

    Q · 01 What is an Aircraft Arresting Gear (AAG) System?
    The AAG is a permanent, high-energy, net-based emergency runway arresting system installed at runway ends to safely stop fighter and tactical aircraft (approximately 6,000-40,000 kg) by converting kinetic energy into heat in a water-glycol energy absorber.
    Q · 02 When would an AAG be used?
    It is deployed for rejected take-offs, landing overruns on wet or low-friction runways, brake or anti-skid failures, crosswind or tailwind mis-touchdowns, high-elevation or hot-day long stopping distances, or when obstacles exist beyond the runway end.
    Q · 03 What are the key performance specifications of the AAG system?
    The system is designed for aircraft of approximately 6,000-40,000 kg, a maximum arresting run-out of up to 270 m depending on entry speed and mass, and controlled peak deceleration of about 3g via a dual-stage absorber.
    Q · 04 How does the AAG arresting concept work?
    On command, two stanchions raise a wide textile net that captures the aircraft. Shear pins release the net anchors so the net travels with the aircraft and pays purchase tape into a dual water-twister absorber that dissipates energy as fluid shear heat, bringing the aircraft to a controlled stop.
    Q · 05 What is the net (MENA) design and strength?
    The Multi-Element Net Assembly (MENA) is approximately 58 m wide and 4.7-4.9 m high, built from 40 vertical high-tenacity Nylon-66 elements. Vertical element strength exceeds 3,400 kgf and horizontal element strength exceeds 2,300 kgf, and the net geometry wraps around the nose and fuselage to spread loads.
    Q · 06 What energy absorber does the AAG system use?
    A dual stacked water-twister energy absorber rated 20T + 40T, using a water plus ethylene-glycol working fluid. Stage selection is actuator-driven in under 5 seconds to tune the torque and deceleration curve.
    Q · 07 How fast does the net deploy and how long does the system take to reset after an arrest?
    Net raise to full arresting height takes about 3 seconds. Tape rewind and full system reset typically take 10-15 minutes, so the runway returns to service quickly.
    Q · 08 What ensures predictable net release and load monitoring in the AAG system?
    Net Anchors (NA) and the Engagement Support System (ESS) use calibrated 2,500 kgf shear pins and suspension/restraining ropes to control release, while tape connectors carry strain-gauge load cells and a DAQ for traceable arrest-load records.
    Q · 09 What standards does the AAG system's tape-handling and sheave hardware meet?
    The Pressure Roller Assembly is designed to meet MIL-B-83183B purchase-tape handling criteria, sheave assembly housings follow IS 9975-1981, and stanchion structural steelwork is fabricated from IS 2062 E250 structural steel.
    Q · 10 What control, power and civil infrastructure does an AAG installation require?
    An Electrical Control System (ECS) with full interlocks, a control hut of approximately 12 x 8 x 3.5 m with UPS and communications (around 6 kW rooftop solar plus DG provision), and dedicated RCC foundations and ducts sized for worst-case dynamic arrest loads.
    Q · 11 What are the maintenance and inspection priorities for an AAG system?
    Scheduled inspection covers the textile net and purchase-tape condition, wire ropes, sheaves, bearings and seals, energy-absorber fluid health (water-glycol), and civil anchor points. Modular subsystems simplify spares management and targeted repairs.
    Q · 12 How can I get a quotation for the Aircraft Arresting Gear (AAG) system?
    You can request a quotation for the Aircraft Arresting Gear (AAG) system by contacting Neometrix Engineering Pvt Ltd through https://neometrixgroup.com/products/aircraft-arresting-gear-system or by phone at +91-7777-876-876.
    Get a proposal

    Tell us your runway
    and aircraft class.

    We scope the net and stanchion layout, size the absorber stages for your aircraft mass range, and walk through installation and civil works with your airfield engineering team.

    Request proposal +91 7777 876 876

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