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HAL PTAE-7

turbofan aircraft engine

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionJun 8, 2026
Entity authorityQ135617910
Source-derived summary

The HAL PTAE-7 (Pilotless Target Aircraft Engine-7) is an Indian small turbojet engine developed by the Hindustan Aeronautics Limited (HAL)

The engine uses a four-stage, axial-flow compressor design with a single-stage turbine. The first stage is transonic. The engine is intended for target drones and other UAVs.

History

In the late September 1980, the development project for indigenous development of PTA Engine (PTAE-7) was sanctioned at an estimated cost of ₹45 million (US$467,291.30) to HAL based on a feasibility study and project proposal submitted by HAL.It was intended to power the DRDO Lakshya Target drone. The engine was fully developed by HAL by September 1985, concurrently with the PTA. HAL announced the successful trial of the indigenously designed and developed remote-controlled PTAE-7 jet engine on 24 January 2001.

The HAL CATS Warrior employs two modified PTAE-7 engines that have been further developed by Aero Engine Research and Development Centre. The modified engine, designated PTAE-W, is a single-shaft, lightweight turbojet engine. The engine measures is 1.27 meters in length, 330 mm in diameter, and weighs 65 kg. The engine core includes a four-stage transonic axial compressor, single-stage turbine, annular flow combustion chamber, and 16 fuel flow burners. The engine variant also features a new FADEC system and an enhanced time between overhauls (TBO) of 1,000 hours with a thrust output of 380 kgf (3.7 kN) and a specific fuel consumption of 1.15 kg/kg.f/hr.

Editorial summary

“HAL PTAE-7” enters the record as turbofan aircraft engine. Crown Archives preserves that source wording while asking what PTAE-7, turbofan and aircraft can confirm, complicate or overturn.

Editorial reviewA concise reference frame for defining the subject, testing terminology and identifying the institution closest to the evidence. The current lead gives the account dated anchors—1980, 1985, 2001—that can be checked directly. The selected authority fields contribute no independent date. Its strongest next move is a source search built around PTAE-7, turbofan and aircraft.
Editorial analysis

Why this record matters

“HAL PTAE-7” is worth following because a concise public description often conceals a longer documentary argument. Here, PTAE-7, turbofan and aircraft provides the most credible route into that argument.

Evidence profile

Vocabulary and entity names are the principal evidence signals here, because they determine the precision of every later search. The source revision retrieved here is dated Jun 8, 2026. The linked authority identifier is Q135617910. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1980, 1985 and 2001.

Critical limits

Overview language is designed for orientation and should not be treated as a substitute for the evidence cited beneath it. The source lead contains qualifying language; that uncertainty should survive quotation, summary and reuse. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

How to read it

Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.

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Source & attribution

This entry incorporates text from HAL PTAE-7” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.