DroneLedger

DRONELEDGER / Press factsheet

IAI Heron / Heron 1

A compact selection from this profile, with sources and limits. Other configurations and additional measurements remain in the full profile.

Full profile and archive

An Israeli medium-altitude reconnaissance aircraft with twin tail booms. The current IAI specification and Singapore’s 2012 Heron 1 fiche differ in length, mass and endurance and remain separate source configurations.[1]

Public-source profile. Performance claims are attributed; type links do not verify an incident identification.

Schematic top view of the general configuration. Not to scale and not an exact depiction of the model.

The numbers, with their sources

Body length8.5 m[1]Heron · current IAI fiche · Publication year unknown · consulted 2026-11-01
Manufacturer claim
Wingspan16.6 m[1]Heron · current IAI fiche · Publication year unknown · consulted 2026-11-01
Manufacturer claim
Take-off mass1270 kg[1]Heron · current IAI fiche · Publication year unknown · consulted 2026-11-01
Manufacturer claim
Payload≤ 470 kg[1]Heron · current IAI fiche · Publication year unknown · consulted 2026-11-01
Published upper limit
Endurance≤ 45 h[1]Heron · current IAI fiche · Publication year unknown · consulted 2026-11-01
Published upper limit

Form, sound & identification limits

Shape or sound alone cannot identify a drone. Follow local public-safety alerts; do not approach wreckage.

Source notebook

  1. Israel Aerospace Industries · Heron: current manufacturer specification

    Publication date not stated · Source consulted: 2026-11-01 · Manufacturer claim

  2. Singapore MINDEF · Fact Sheet: Heron 1 UAV

    2012-05-23 · Source consulted: 2026-11-01 · Official report; not an independent test

Cite this profile

DroneLedger. IAI Heron / Heron 1. 2026-11-01. https://droneincidents.com/drones/iai-heron-1/editions/2026-11-01/

Our text, data and schematic drawings: CC BY 4.0, credit DroneLedger and link to the profile. Linked publications and quoted passages keep their own rights.