BlueCap Australia

BlueCapHeli® — long-endurance petrol drone helicopter

BlueCap operates three-helicopter BlueCapHeli® survey systems with three pilots for magnetic, LiDAR and radiometric surveys. Two complete teams can be scoped on request for roughly twice the daily magnetic line-km in suitable conditions.

BlueCapHeli® petrol drone helicopter prepared for a geophysical survey

BlueCap-operated airborne carrier · designed in Australia

BlueCapHeli® carries magnetic, LiDAR, radiometric and imaging payloads over large, remote and rugged survey areas.

BlueCap’s standard survey system is three BlueCapHeli® helicopters with three pilots. The aircraft usually fly in parallel; a very small block may use two at once when BlueCap’s operational plan calls for it. Clients purchase the complete survey service rather than selecting an aircraft count. Two complete teams, six helicopters and six pilots in all, can be scoped on request for roughly twice the daily magnetic line-km on a suitable project; the quote and flight plan are assessed separately.

The aircraft, payload, remote pilots, field communications and processing workflow are delivered as one BlueCap survey service. BlueCapHeli® is not sold or leased as standalone equipment. In international specifications, the same fuel class may be described as a gasoline-powered or gas-powered drone helicopter; Australian copy uses petrol.

BlueCapHeli® survey helicopter showing its single-rotor airframe and field configuration
Designed in Australia · manufactured in-house in Perth, WA

Two tanks. One survey aircraft. The mission selects the endurance.

The 3.2 L configuration supports compact survey cycles and quick field service. The 10 L configuration provides additional mission-design margin for remote polygons, long transit legs and extensive production lines. A larger tank is not automatically the better survey plan.

BlueCap-operated survey aircraftThe platform is integrated with the payload, flight crew and data workflow. It is not sold or leased as standalone equipment.
3.2 L configurationUp to 3 h

Current compact fuel cycle

Selected when payload, polygon, operating point, reserve and planned service stops fit a shorter sortie.

10 L configurationUp to 8 h

Long-endurance fuel cycle

Evaluated when distance to the survey block or long production lines would make frequent returns inefficient.

≈2.5 m

overall airframe length

The aircraft is almost two and a half metres long, giving clients a clear physical scale well beyond a typical electric survey multirotor.

≈100 km/h

normal survey speed

Maximum cruise is 140 km/h. For radiometric acquisition BlueCap can hold a stable 20 km/h terrain-relative flight profile when required by the measurement plan.

25 kg

registered category

CASA single-rotor liquid-fuelled helicopter category up to 25 kg; the approved mission configuration remains controlling.

8.8 kg

dry mass

Aircraft mass before fuel, payload and other mission-specific equipment are added.

≈29 kg

maximum static lift

The upward force measured while the helicopter is held in place. It shows lifting capability; approved take-off mass still sets the usable fuel and payload.

Petrol propulsionEngine-driven generatorSmart Li-ion flight power

A hybrid onboard power architecture keeps the aircraft battery charged in flight without implying electric rotor propulsion. The flight battery does not need to be removed or charged between fuelled missions.

Engineered as a connected survey carrier — not a bare airframe

BlueCap designed and developed the platform in Australia between 2023 and 2026 and has manufactured it in-house in Perth, WA since 2025. Each aircraft is configured around the payload, terrain, communications coverage and approved operating plan.

BlueCapHeli® engineering configuration viewed during field preparation
01Rotorcraftsingle-rotor control authority
02Petrol enginelong-duration energy source
03Payload interfacemagnetic · LiDAR · gamma · imaging
One carrier configured around the approved payload and survey geometry
Layered operational safety

More people can supervise. More than one path can bring it home.

BlueCapHeli® keeps approved-route execution, independent oversight and the direct-radio contingency path distinct.

Approved-route lockNo arbitrary point-and-fly control

No user can steer or redirect the helicopter to an arbitrary location. It flies only the route agreed and approved before take-off; authorised intervention is limited to permitted safety actions such as Stop Mission and Return-to-Base.

01 · authorised oversight

Live, log and replay visibility

Authorised aviation regulators and airspace controllers can observe the aircraft in real time, inspect its flight logs and replay recorded missions. Where operational authority requires intervention, approved access can stop the survey mission and initiate Return-to-Base, but never redirect it to an arbitrary destination.

02 · routine command path

Encrypted internet control

BlueCapHeli® does not rely on a conventional handheld transmitter and does not accept point-and-fly steering. BlueCap pilots supervise the approved mission and issue only permissioned commands through redundant encrypted internet channels, with fingerprint confirmation for critical actions.

03 · independent contingency

Direct RF Return-to-Base

A restricted direct-radio controller remains available over approximately 10–15 km line-of-sight. It is not a manual steering handset: in an unforeseen situation it can issue Return-to-Base directly, taking priority over the internet control path.

Priority pathDirect RFAircraft
Adaptive engine management

Smart fuel–air control for real survey terrain

Survey terrain can change engine conditions by hundreds of metres inside one project. BlueCap built the control response for the climb, descent and changing air density that follow.

01 04
The field problem

One survey. 600–800 m of elevation change.

Geophysical survey lines often cross ridges, valleys and escarpments where elevation changes by 600–800 metres inside one project area.

A petrol engine tuned at take-off does not encounter the same air density hundreds of metres higher or lower. One manual setting can become too rich, too lean, too hot or unstable as the aircraft follows the terrain.

  • ridges · valleys · escarpments
  • 600–800 m project relief
  • changing air density
01

Interchangeable survey payloads

BlueCapBird® magnetometers, Medusa gamma spectrometers, BlueCapLidar® and imaging systems are integrated as project configurations.

02

Active payload altitude

BlueCapWinch® provides motorised real-time control of a suspended sensor independently of the carrier's immediate vertical motion.

03

Airspace visibility

A 9 W aviation-grade high-intensity LED strobe supports operational visibility and the applicable aviation-safety plan.

Flight platformPayload integrationField connectivityControlled data chain
Low-noise petrol flight03

Petrol endurance. Electric-drone-like sound levels.

BlueCap developed an innovative exhaust silencer that substantially reduces the normal acoustic presence of a petrol engine. The result is a long-endurance survey helicopter that remains close to an electric heavy-lift drone in BlueCap's same-condition hover measurement.

BlueCap comparative hover measurementHover · measured at 20 m · same conditions
Petrol + silencer71 dB

BlueCapHeli® with the engineered silencer

6 dB measured difference
Electric reference65 dB

DJI Matrice 600 Pro under the same conditions

BlueCap measured both aircraft on the same test basis. These figures are comparative field measurements, not a statutory acoustic certification.

People nearby

The quieter exhaust is less intrusive around communities and work crews and avoids a persistent petrol-engine note becoming a nuisance during long survey programmes.

Animals and wildlife

Lower acoustic presence helps reduce avoidable startle and disturbance around livestock and wildlife while the project flight plan retains its site-specific controls.

Long field days

Lower noise exposure reduces fatigue for pilots, spotters and field personnel working near the operating base across repeated survey sorties.

Long-endurance petrol flight does not have to sound like a conventional petrol aircraft. BlueCapHeli® combines its engineered exhaust silencer with the mission endurance required for commercial geophysical survey.

A complete survey system, ready for field work

One BlueCapHeli® survey system comprises three helicopters and three pilots. Two complete teams can be scoped on request for roughly twice the daily magnetic line-km in suitable conditions. Useful line-kilometres still depend on survey geometry, terrain, payload behaviour, weather, approvals and field QC.

Two fully assembled BlueCapHeli® survey helicopters prepared together in the field
Survey-ready fleet5fully assembled, flight-ready helicopters
Complex-mission deployment: three primary flying aircraft plus two complete, immediately available backup aircraft.
Nearly 400 h

combined fleet flight time

The accumulated BlueCapHeli® flight history spans aircraft development, testing, trial programmes and commercial survey operations.

1,800–2,400

line-km / flying day / system

Three helicopters typically acquire 600–800 productive line-km each. Nominal planning is 2,100 per system-day, subject to geometry, payload, terrain, turns, weather, approvals and field QC.

One repeatable field cycle

Prepare once. Acquire useful lines. Service quickly. Continue.

  1. 01
    Pre-flight configurationairframe · payload · links · reserve
  2. 02
    Productive acquisitiontransit · survey lines · controls · turns
  3. 03
    Quick-swap tankless than 5 minutes in the comparison basis
  4. 04
    Field QC and next sortieaccept · repeat · adapt the plan

Campaign rebuild

Before a new survey campaign, each helicopter is disassembled, inspected and rebuilt; uncertain or worn components are replaced before deployment.

Mission continuity

Flight-ready backup capacity supports continuity when an aircraft needs maintenance or replacement.

Continuous oversight

Remote pilots monitor aircraft systems, payload behaviour and onboard sensors rather than treating autonomy as unattended operation.

Scalable control

Secure pilot handover and multi-aircraft coordination are supported where staffing, permissions and the approved plan allow them.

The client outcome is the protected delivery schedule. Endurance, backup aircraft, in-field maintenance and QC are useful only when they keep acceptable data moving through the programme.

Same survey. Fewer field days. Lower delivery cost.

This comparison is based on BlueCap's late-2025 field experiment with the same suspended BlueCapBird® magnetometer. Results from the DJI Matrice 600 and BlueCapHeli® are normalised to one identical 9 × 8 km client deliverable so field duration, aircraft programme time and direct team cost can be compared on the same survey basis.

BlueCap-operated DJI Matrice 600 Pro in flight carrying survey equipment
Battery multirotor systemDJI Matrice 600 Pro
BlueCapHeli® petrol drone helicopter flying an airborne survey over tropical highland terrain
Purpose-built survey carrierBlueCapHeli®
One common client deliverable

9 × 8 km magnetic drone survey

72 km² · 50 m production-line spacing · 1,440 accepted line-km · eight airborne hours per day · five minutes for each landing, energy service and next take-off.

8 airborne hours per day

Field deployment

Matrice 6006 days
BlueCapHeli®3 days
BlueCapHeli® wins · 50% fewer field days
total aircraft programme time

Flight + energy service

Matrice 60053 h 42 min
BlueCapHeli®17 h 32 min
BlueCapHeli® wins · 67% less programme time
A$1,200 per person-day

Direct field-team cost

Matrice 600A$19.8k
BlueCapHeli®A$7.2k
BlueCapHeli® wins · 64% lower team cost
Commercial parameterMatrice 600BlueCapHeli®
Client deliverable · magnetic drone survey · 9 × 8 km · 1,440 line-km
Field duration6 days3 days
Flight + energy service53 h 42 min17 h 32 min
Team on site (spotters excluded; equal numbers for both systems)3 people · 16 person-days2 people · 6 person-days
Direct field-team costA$19,800A$7,200
Field energy support66 batteries · 11 chargers · 7.5 kW petrol generatorFuel service · no field charging station

Comparison basis. Late-2025 BlueCap field-experiment data informs both aircraft. The Matrice 600 result uses its measured accepted production rate and observed landing and battery-service cycle; the BlueCapHeli® result applies the same survey geometry and field-day basis to BlueCapHeli operating data. These fixed values describe this experiment basis and are not a fixed quotation.

BlueCapHeli® versus a crewed Bell 206 on the same survey grid

This planning comparison holds survey area and production-line spacing equal. It then compares a Bell 206 crewed helicopter with BlueCapHeli® while keeping their different certification, crew, autonomy, clearance and logistics profiles visible.

Bell 206 JetRanger used as a crewed survey-aircraft planning reference
Crewed benchmarkBell 206Established airborne-geophysics operating model
BlueCapHeli remotely piloted geophysical survey helicopter
Remotely pilotedBlueCapHeli®Low-altitude, field-scalable survey model
Indicative fuel consumption
Bell 206~110–120 L/h
BlueCapHeli®~1.1–1.2 L/h
BlueCapHeli® wins · about 99% lower indicative hourly fuel consumption
MetricBell 206BlueCapHeli®
Survey flight speed~80 km/h~100 km/h
Maximum climb≈5.8 m/s≈18.1 m/s
Maximum descent≈8 m/s≈15 m/s
Low-altitude comparison basisTypically 120–200 m AGLPrecision terrain following below 45 m where approved
Endurance≈3 h on full fuel≈3 h with 3.2 L · up to 8 h with 10 L
Refuelling / tank service≈30 min<5 min
Crew exposureOnboard human pilotRemotely piloted from the ground
Field logisticsFuel truck or mobile tank and certified supportPortable RON 91 petrol and in-house field service
Magnetic data geometry

The sensor and drape profile shape the recorded anomaly

Both aircraft can carry 1–3 pT-class magnetometers. Sensitivity alone does not control spatial resolution.

BlueCap Portal 3D terrain simulation showing calculated survey routes over mountainous terrain
3D terrain simulationRoute design against the DEMInspect the calculated aircraft path, terrain and mission state before field deployment.
01 / 02
More consistent clearancesupports cleaner anomaly amplitudes and more confident target ranking
Planning basis, not a universal aircraft claimActual clearance and control depend on terrain, payload, approvals and the mission system used.

Safety planning starts with the consequence of failure

The question is not whether an aircraft can fail. It is how the particular airframe is maintained and tested, what recovery modes remain available, how energy-source hazards are controlled and how people, infrastructure and dry country are protected.

Loss of engine power

Autorotation changes the descent outcome

FAA diagram comparing downward rotor airflow in normal powered flight with upward airflow through the rotor during autorotation

With rotor and flight-control authority available, airflow can keep the rotor turning and retain directional control toward a suitable touchdown area. It reduces descent severity; it does not guarantee an incident-free landing.

Energy-source consequence

Petrol and Li-Po require different controls

Petroldoes not self-heat after impact; leaked fuel is contained and kept away from open flame and other ignition sources
Li-Poimpact damage can short cells and initiate self-sustaining thermal runaway

Across years of BlueCapHeli® operations, BlueCap has never recorded a helicopter fire. Remote pilots and spotters are trained for fuel and fire response, and spotters carry fire extinguishers in the field. Petrol and Li-Po still require different prevention, isolation and emergency procedures.

Specific-airframe validation

Emergency modes are tested before production sorties

Deliberate checks are performed at safe altitude over a prepared area. The aircraft proceeds only after the required modes are verified.

  1. 01Engine shutdown / partial power loss
  2. 02Datalink loss / loss-of-control scenarios
  3. 03Actuator and drive jamming simulations

Newly built or freshly assembled

Each project receives a newly built or freshly assembled and tested aircraft rather than an airframe with uncertain component condition.

Pre-survey autorotation test

A deliberate in-flight engine-shutdown procedure is completed before the aircraft is cleared for production work.

Defined stop criteria

Weather, communications, payload behaviour, reserve, landing options and exclusion zones remain explicit reasons to stop or alter a sortie.

Project-specific aviation case

The controls support the survey HSE plan; they do not replace CASA permissions, site controls or the risk assessment for the actual project.

BlueCap project-fit review

Start with the polygon, payload and operating environment

BlueCap will assess fuel configuration, useful endurance, terrain, communications, reserve, payload geometry, aviation approvals and required survey products before selecting the aircraft plan.

Discuss the aircraft configuration

Related systems: BlueCapBird® quantum magnetometer payload, BlueCapLidar® dual-scanner payload, magnetic survey service and LiDAR survey service.

One planned field day · published planning values

Watch one planned field day fly itself

Press play to see one three-helicopter BlueCapHeli® survey system acquire a schematic block. The counter illustrates a nominal 2,100 productive line-km on a suitable flying day. The aircraft count shown is an explanation of the standard system, not a customer selection.

One BlueCapHeli® survey system

Three helicopters and three pilots normally operate together. BlueCap sets the aircraft plan; clients do not select an aircraft count.

Local time · eight-hour field day
08:00day flown 08:00 → 16:00
Productive line-km
0of ≈2,100 line-km/day
Pilots
3for the standard system; other field roles depend on survey scope

Project enquiry

Let’s plan your survey

Start with your survey area and the data you need. We’ll help define the scope, review terrain-aware 2D and 3D flight plans, and keep field progress, processed data and deliverables together in the BlueCap Survey Portal.

No software subscription fee for BlueCap service projects.

Inside the Portal01 / 07
BlueCap Portal map showing a large survey polygon divided into coordinated routes for four aircraft sorties
Multi-aircraft survey allocationDivide a large survey area into coordinated aircraft sorties and review the complete route geometry on the map.