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ANEP-83

ANEP-83 shipborne helicopter and UAV harpoon-grid securing system

Naval engineering authorities, shipyards and harpoon designers in NATO nations that build or fit a shipborne helicopter or UAV harpoon-grid securing system, under the agreement recorded in STANAG 1276

ANEP-83 sets NATO's mandatory harpoon and grid interface dimensions, tolerances and mechanical characteristics for securing a helicopter or a VTOL UAV to a ship's flight deck, and it binds nations through the agreement recorded in STANAG 1276.

Edition
A
Published
2014-06
THIS DOCUMENT Agreement Holds requirements Organisation certificate Product or design assessed ALLIED NAVAL ENGINEERING PUBLICATION · EDITION A · 2014-06 ANEP-83 Shipborne helicopter and UAV harpoon-grid rapid securing system ANEP-83 sets NATO's mandatory harpoon and grid interface dimensions, tolerances and mechanical characteristics for securing a helicopter or a VTOL UAV to a ship's flight deck, and . AGREEMENT STANAG 1276 The agreement that puts this publication into force. WHERE THE REQUIREMENTS LIVE ANEP-83 ANEP-83 sets NATO's mandatory harpoon and grid interface dimensions, tolerances and mechanical characteristics for securing a helicopter or a VTOL UAV to a ship's flight deck, and . A supplier meets ANEP-83 when a contract or national instruction names it, usually via STANAG 1276. Addressed to national authority, designer. Covered by STANAG 1276. ANEP-83 sets mandatory and example mechanical characteristics for a shipborne harpoon-grid securing system. Reaches a supplier when a contract, tender or national instruction names it. Nobody is certified against this document. Nations report ratification; they do not issue a company certificate.

What it is

ANEP-83, printed on its own cover as ANEP/MNEP-83, is a NATO Allied/Multinational Naval Engineering Publication: the technical document that fixes the mandatory mechanical characteristics of the harpoon-grid rapid securing system used to hold a helicopter or a VTOL UAV to a ship's flight deck immediately after touchdown and until take-off. Its aim is to enhance the safety of these interoperations between aircraft and ships, and to prevent nations developing new systems that would not interoperate with the harpoon-grid systems already in service (clause 1).

It is narrower than a full grid specification. The document provides guidance for honeycomb design, but its primarily intention is not to specify a grid for ship construction (clause 2): each nation still describes and publishes its own grid's overall shape and construction data separately, within a companion publication it calls MPP-02. What ANEP-83 fixes as mandatory is the shared interface, the geometry that lets any compliant harpoon engage any compliant grid regardless of which nation built either one.

The harpoon and the grid

A harpoon-grid rapid securing system secures a helicopter or a UAV to the flight deck by extending a harpoon telescopically under the fuselage, engaging its jaw into one of the grid's holes, then locking and retracting to hold the aircraft down under tension; disengagement unlocks and retracts the harpoon again (clause 3). The grid itself is a stainless steel plate machined into a honeycomb of calibrated holes, normally flush with the deck, with an omnidirectional network of isthmus that the harpoon's claws secure onto (clause 3.3).

What the harpoon must do (clause 4.1)

The harpoon must engage and disengage on an isthmus with an 80 mm clearance height under the grid; have mechanical and metallurgic characteristics compatible with the grid's own material properties; carry a built-in mechanical fuse that breaks once it reaches a specified tension, so an overload shears the fuse rather than damaging the deck or the aircraft; and engage regardless of the helicopter's heading.

The grid's mandatory dimensions (clause 4.2)

Working from the grid-detail drawing at figure 6.3, clause 4.2 fixes the honeycomb's own geometry:

  • Top plate thickness: 28 mm, +1.5/-0.5 mm
  • Extent of harpoon engagement: 92 mm
  • Honeycomb hole diameter: 51 mm, theoretical
  • Distance between two holes: 66 mm, ± 0.5 mm
  • Isthmus width: 15 mm, ± 0.5 mm
  • Isthmus height: less than 27 mm
  • Minimum height between the top and lower plate: 80 mm

This is the interoperability layer: get any one of these wrong and a harpoon built to one nation's tolerances will not reliably engage a grid built to another's.

Example load and material figures (clause 5)

Clause 5 is optional rather than mandatory: the grid should be at least capable of withstanding constraints in accordance with the heaviest helicopter likely to operate on the deck, and the document gives worked examples, not one universal figure, across a UAV-VTOL, a light helicopter and a medium helicopter:

  • Harpoon tension without permanent distortion: 3,000 daN for a UAV-VTOL, 4,000 daN for a light helicopter, 8,500 daN for a medium helicopter
  • Landing gear reaction load: 4,000 daN, 7,100 daN and 21,000 daN across the same three classes
  • Minimum ultimate tensile strength: above 900 MPa for a UAV-VTOL or a light helicopter, above 1,300 MPa for a medium helicopter
  • Minimum core Rockwell hardness: 28 HRC for a UAV-VTOL or a light helicopter, above 40 HRC for a medium helicopter

A nation picks the class, and the figures that go with it, that match the heaviest aircraft its own deck expects to operate. The remaining clause, 6, is drawings rather than requirements: an illustration of a harpoon locked into a grid, a general grid display, the grid-detail dimensions drawing clause 4.2 refers to, and an enlargement of the grid.

Who it binds, and how

ANEP-83 does not address individual aircrew or shipboard operators directly. Its own terms point to the nations that approved it through the Military Committee Maritime Standardization Board, and to whichever national authority, shipyard or harpoon designer specifies the equipment. Nations agree to use the publication through the agreement recorded in STANAG 1276; it binds a nation's own naval engineering authority once that nation has taken the agreement on, and it reaches a shipyard or a designer because that authority specifies it, not because NATO printed the document. Edition A, Version 1 was promulgated 25 June 2014 and is effective upon receipt; the document does not say what, if anything, it superseded.

How it is evaluated

ANEP-83 describes no certification, audit or inspection scheme, and names no accredited body, notified body or government surveillance role. What exists is a set of mandatory figures in clause 4 and example figures in clause 5; checking a specific harpoon or grid design against them is left to whichever national naval engineering authority or shipyard specifies and accepts the equipment.

Getting the document

NATO publishes ANEP-83 through the NATO Standardization Document Database at no charge. ComplyTrain does not sell it or host a copy; the NSDD listing for ANEP-83 is the source. It is covered by STANAG 1276, the agreement recording nations' commitment to use it.

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How we help

ANEP-83 is a mechanical engineering interface standard. The work it demands, fixing a harpoon's and a grid's clearances, tolerances and material properties, and verifying a specific design against them, is naval architecture and mechanical engineering, not something a compliance platform performs.

What ComplyTrain supports is the paperwork trail around that engineering work: holding the design and verification records that show a harpoon or a grid was specified against clause 4's mandatory characteristics, the national data a nation submits for MPP-02, and the revision history and sign-offs behind them, kept current and ready to produce for a customer or a national authority.

What ComplyTrain does not do: it does not design, machine, test or accept a harpoon or a grid, and it does not decide which of clause 5's weight-class figures a nation should specify for its own ships. See where ANEP-83 sits alongside STANAG 1276 and other maritime publications in the standards explorer, and talk to us about the design and verification record trail behind it.

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Tell us how you need to work with ANEP-83 and what you need from it. We will come back to you about what ComplyTrain can do.

Questions

Is ANEP-83 mandatory?

Not by itself. ANEP-83 is covered by STANAG 1276, the agreement recording nations' commitment to use it. Whether it applies to a specific ship or aircraft programme depends on whether the operating nation has taken on that agreement and specifies ANEP-83 in its own naval engineering requirements.

Does ANEP-83 specify the whole grid?

No. Its stated intention is not to specify a grid for ship construction. It fixes the interface dimensions in clause 4, the geometry a harpoon and a grid must share, and leaves each nation to describe and publish its own grid's overall shape and construction data separately, in a publication it calls MPP-02.

What is the difference between the mandatory and the optional characteristics?

Clause 4's harpoon and honeycomb dimensions apply to every compliant system. Clause 5's load and material figures are worked examples a nation uses to size a grid to its heaviest expected aircraft, scaled across a UAV-VTOL, a light helicopter and a medium helicopter, rather than a single fixed requirement.

Does ANEP-83 cover UAVs as well as helicopters?

Yes. The document defines the harpoon-grid system as securing "a VTOL aircraft (Helicopter or UAV)" to the flight deck, and clause 5's example mechanical characteristics give a separate UAV-VTOL class alongside light and medium helicopter classes.

Who checks that a harpoon or a grid meets ANEP-83?

The document does not say. It sets the mandatory and example figures but names no accredited body, notified body or government surveillance role; checking a specific design against them is a matter for whichever national naval engineering authority or shipyard specifies and accepts the equipment.

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