Role & capabilities
- Onboard observation
- Alternative propulsion configurations
- Containerised launch offering
- Primary domain
- Air
- System type
- Loitering munition
- Developer / manufacturer
- Global Industrial & Defence Solutions
- Origin / production countries
- Pakistan
- Other names
- No additional names recorded
- Variants / configurations
- Yalghar 100; Yalghar 500
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Current source identifies 100 and 500. Other numbers appearing in secondary family descriptions are not assumed to be equivalent variants.
GIDS now presents Yalghar as a family with two named baseline configurations. Yalghar 100 is electrically powered and uses a cruciform wing-and-tail arrangement. The larger Yalghar 500 uses gasoline propulsion. Both are described as canister-launched systems with observation sensors and a control link.
The manufacturer's present table supplies distinct mass, endurance and range figures for each version. Those values should stay attached to the relevant model; the family name is not evidence that the two aircraft have identical propulsion or performance. Published range is also not automatically the radius of a particular mission or the distance over which every sensor function is available.
The product page establishes an offering, but does not identify a recipient, an acceptance date or an independently documented deployed fleet. Claims about autonomy remain supplier descriptions. This entry therefore records Yalghar's public design distinctions while leaving service history and validated production configurations open.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Airframe | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Launch / recovery | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Propulsion | Yalghar 100: electric; Yalghar 500: gasoline | Supplier specification; no independent performance validation established. Source |
| Dimensions | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Mass | Yalghar 100: 55–60 kg; Yalghar 500: 82 kg | Source labels these as weight, without a detailed configuration definition. Source |
| Endurance | Yalghar 100: 90 minutes; Yalghar 500: over 150 minutes | Supplier specification; no independent performance validation established. Source |
| Range | Yalghar 100: 100 km; Yalghar 500: 500 km | Manufacturer maximum-range claims; definition and flight conditions unspecified. Source |
| Speed | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Altitude | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Payload | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Sensors | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Communications / navigation | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
Publication history
- — Published reference update.
Suggest a correction to this entry
Follow the evidence
Source types identify who makes the claim. Programme milestones and supplier statements should be read in context.
- GIDS Yalghar current product page (opens in a new tab)Manufacturer / programme