BlueCap Australia

Drone Radiometric Survey

BlueCap drone radiometric surveys use the Medusa MS-1000 gamma-ray spectrometer to deliver traceable K, eU, eTh and total-count mineral mapping.

Medusa MS-1000 gamma-ray spectrometer with carbon-fibre housing and blue electronics head

BlueCap delivers drone radiometric survey and gamma-ray mapping services for mineral exploration across Australia and worldwide. Low-level mission design, Medusa MS-1000 acquisition, spectral processing and reviewable K, eU, eTh and total-count products remain inside one BlueCap-operated workflow.

Medusa MS-1000 in one BlueCap survey system

BlueCap integrates the Medusa Radiometrics MS-1000 gamma-ray spectrometer with the aircraft, mission design, field crew, live detector view and controlled data workflow. The client commissions a survey and defined geological products — not an unsupported sensor rental.

Passive gamma-ray spectrometryThe detector records naturally occurring radiation; it does not transmit gamma energy into the ground.
BlueCapHeli® airborne geophysical survey platform in flight preparation
Medusa MS-1000 payload integrated with the BlueCap airborne survey platform
011000 ml

CsI crystal

BlueCap integrates the 3 × 9 inch shock-resistant scintillation detector as part of the complete airborne system.

026.7 kg

Sensor mass

The complete mission payload must also include mounting, cabling, power and integration hardware.

035 Hz

Recording rate

The system records five spectra per second; this does not mean five statistically independent final maps every second.

04100 × 375 mm

Detector envelope

The physical envelope is included in BlueCap mounting, balance, clearance and aircraft-integration checks.

0516 GB

Internal storage

Onboard capacity provides substantial headroom for long field records while project data is also controlled through the BlueCap workflow.

06IP65

Instrument protection

BlueCap plans inside the instrument operating range of −20 to +65 °C while applying separate aircraft and mission weather limits.

01

BlueCapHeli® model integration

The MS-1000 is integrated into BlueCap's 3-hour and 8-hour BlueCapHeli® models. Mounting, balance, vibration, airflow, 25 V power, communications, landing clearance and safety are qualified as complete aircraft configurations.

02

1000 ml CsI detector

The scintillation crystal records the energy distribution of gamma photons with the efficiency required for drone-scale ground mapping.

03

mDOS field view

Detector storage and near-real-time review support acquisition checks and reflight decisions without replacing final processing.

04

Traceable handover

Source spectra, position, processing parameters, grids, tables, QC decisions and exceptions remain connected in the project record.

BlueCapHeli® carrierMedusa MS-1000mDOS field viewTraceable delivery

Why BlueCap integrates the Medusa MS-1000

A larger scintillation volume can improve count statistics when geometry and integration time are equal. It also consumes payload margin and can change speed, altitude or endurance. BlueCap therefore compares detector material and volume, flight-installed mass, synchronisation and quality control together — not model name or kilograms alone.

BlueCapHeli® payload screen9.5 kg

BlueCap selected and integrated the MS-1000 for its current service configuration. Within the MS-700, MS-1000 and MS-2000 family, it provides the largest detector volume that remains within BlueCapHeli®'s 9.5 kg payload screen at a 6.7 kg instrument mass.

  1. Smaller Medusa class

    Medusa MS-700

    4.7 kg

    700 ml CsI · 3 × 6 inch

    Mass basis
    Instrument mass is 4.7 kg. Mount, cable, power and mission hardware still require a complete flight-installed mass check.
    Data chain
    mDOS, GammAn, GNSS/PTH, 16 GB storage, JSON/NMEA/CSV and 5 Hz recording in the Medusa ecosystem.
    Project meaning
    About 2.0 kg lighter than the MS-1000, with 300 ml less CsI volume. It can suit an integration where payload margin matters more than detector size.
    9.5 kg screen
    Below the screen at instrument level; the complete installed configuration must still be weighed and qualified.
  2. BlueCap integrated configuration

    Medusa MS-1000

    6.7 kg

    1000 ml CsI · 3 × 9 inch

    Mass basis
    Instrument mass is 6.7 kg. BlueCap separately accounts for mounting, cabling, power, communications, balance and operational margin.
    Data chain
    1000 ml CsI, GNSS/PTH, internal storage, mDOS and GammAn form a field-to-processing chain BlueCap has integrated and qualified.
    Project meaning
    The selected balance of useful detector volume, aircraft payload margin, traceable data and practical low-level drone operation.
    9.5 kg screen
    The 2.8 kg arithmetic difference is not confirmed spare payload after integration; the complete aircraft configuration remains the engineering basis.
  3. Larger Medusa class

    Medusa MS-2000

    11–12 kg

    2000 ml CsI · 90 × 310 mm

    Mass basis
    Instrument mass is 11–12 kg, already above the payload screen before integration hardware is added.
    Data chain
    mDOS, GammAn, GNSS/PTH and 16 GB storage, in a configuration positioned primarily for vehicle-mounted survey work.
    Project meaning
    Double the MS-1000 detector volume does not make the system flight-compatible when the instrument alone exceeds the aircraft payload screen.
    9.5 kg screen
    Does not pass BlueCapHeli®'s initial 9.5 kg payload screen.
Comparison context

Two external instruments for context, not a purchasing ranking

RS-530 and GS-1 are lighter instruments, but their detector material, volume, aircraft platform, software and integration basis differ. The comparison explains engineering trade-offs; it does not assume the systems will produce equivalent results.

External drone instrument

Radiation Solutions RS-530

3.0 kg

0.39 L NaI(Tl) · 3 × 3 inch · K, U and Th spectral system

Mass basis
The detector and spectrometer assembly is 3.0 kg. A complete common-basis flight mass for mount, cable, CPU, GNSS and external power is not itemised.
Data chain
12 keV–3 MeV range, natural-radioelement stabilisation, embedded GPS and RadAssist altitude correction and NASVD tools.
Project meaning
A lighter instrument with a smaller, different detector and data environment. Mass alone cannot demonstrate equivalent data quality or production.
Comparison gap
A complete flight-installed comparison on the same mass basis remains unverified.
External drone payload

Geoscan GS-1

2.6 / 2.8 kg

0.34 L NaI(Tl) or 0.40 L CsI(Tl)

Mass basis
The NaI(Tl) version is 2.6 kg and the CsI(Tl) version is 2.8 kg. A complete integration inventory on the same basis as BlueCap's configuration remains unverified.
Data chain
30 keV–3 MeV range, internal storage, IP67 protection and field software in the Geoscan 401 Gamma system.
Project meaning
A lighter drone payload with a smaller detector and its own aircraft and data chain, not a direct substitute for BlueCap's MS-1000 workflow.
Comparison gap
Instrument mass is below 9.5 kg, but the complete integration and equivalent synchronised QC fields are not established on a common basis.
  • Useful count statisticsDetector material and volume are considered with altitude, speed, integration time and the required spatial product.
  • Installed flight massInstrument mass is only the start; mount, cable, power, communications, balance and safety margin all count.
  • Synchronised recordSpectrum, GNSS, pressure, temperature, humidity and aircraft geometry must remain traceable by observation time.
  • QC and deliverablesCalibration, corrections, reflight decisions, K–eU–eTh products, metadata and interpretation limits are agreed before mobilisation.

BlueCap does not sell or lease the MS-1000 or the instruments shown for comparison. BlueCap delivers an integrated drone radiometric survey service — mission design, acquisition, processing, quality control and agreed geological products.

From a gamma spectrum to K, eU and eTh maps

The MS-1000 records a full gamma-energy spectrum at each observation. Calibrated window analysis or Full Spectrum Analysis can estimate the relative contribution of potassium, equivalent uranium and equivalent thorium, together with total count and agreed ratio products.

K40K

Potassium

Can help distinguish lithologies, potassium-rich alteration or surface materials where the geological contrast is strong enough and independently checked.

eU238U decay series

Equivalent uranium

A radiometric estimate based on decay products and equilibrium assumptions — not a direct uranium assay or radiation-safety determination.

eTh232Th decay series

Equivalent thorium

Can support mapping of parent material, regolith and lithological variation while remaining sensitive to surface conditions.

TCDefined energy range

Total count and ratios

Total count and ratios such as K/eTh, eU/eTh or eU/K can highlight contrasts when calibration, corrections and metadata remain intact.

Geological questions

Where radiometric contrast can add context

Lithological boundaries

Compare surface units whose radioelement signatures differ enough to complement field mapping.

Alteration context

Test potassium or ratio patterns against an alteration model rather than treating colour contrast as mineralisation.

Regolith and parent material

Add context to weathering, transported cover and near-surface material changes alongside terrain and samples.

Uranium screening

Identify near-surface radiometric contrast for specialist follow-up without replacing assay, equilibrium review or safety controls.

Standard IAEA energy windows · illustrative spectrum

Click a channel and see where it lives in the spectrum

Each mapped element is estimated from a standard energy window on the recorded spectrum. Select a channel to highlight its window and the photopeak it is anchored to.

0.51.01.52.02.53.0Gamma energy (MeV)
Illustrative spectrum shape for reading the windows — not project data.
1.37–1.57 MeV · K-40 at 1.46 MeV

Potassium is measured directly from its own K-40 decay. In mapping it responds to potassium feldspar, micas and potassic alteration — a primary vector in many hydrothermal systems.

Ternary radiometric map of Australia combining potassium in red, thorium in green and uranium in blue from more than 600 merged airborne gamma-ray surveys
All three channels on one map: the ternary Radiometric Map of Australia — K red, Th green, U blue. Radiometric Grid of Australia (Radmap) v4 2019, © Commonwealth of Australia (Geoscience Australia), CC BY 4.0.

Windows follow the standard IAEA airborne gamma-ray spectrometry convention — potassium at the 1.46 MeV K-40 photopeak, equivalent uranium at the 1.76 MeV Bi-214 photopeak, equivalent thorium at the 2.62 MeV Tl-208 photopeak. The drawn spectrum is an illustrative shape for reading the windows, not project data.

Low, slow and designed for enough counts

Productive area cannot be separated from gamma count statistics. Aircraft speed, terrain clearance, line spacing, footprint, background concentration and required map resolution must be designed together before line-kilometres or daily production are quoted.

BlueCap Survey Portal 3D flight simulation of terrain-following acquisition over the survey block
BlueCap holds a 35 m terrain-relative detector clearance and 18 ±1 km/h ground speed; the required line spacing is confirmed before flight.
BlueCap acquisition AGL35 m

Our terrain-following setpoint keeps the detector above typical tropical and subtropical tree height while preserving useful near-surface response.

Client-selected line spacing25 / 50 m

Clients normally select 25 m or 50 m lines for the required product. In some cases, 100 m spacing is used for draft mapping.

BlueCap mapping speed18 ±1 km/h

Stable terrain-relative ground speed balances productive area with consistent spectral acquisition; 20 km/h is the sensor operating maximum.

Recording5 Hz

The detector records five spectra per second; count uncertainty and processing determine usable information density.

Detector enduranceUp to 8 h

BlueCap treats detector power endurance separately from each BlueCapHeli® flight leg, fuel plan and total mission duration.

Integrated power25 V

BlueCapHeli® supplies a controlled 25 V feed to the integrated detector, with approximately 3 W average and 6 W maximum demand.

BlueCap operating point

Area, spatial resolution and spectral certainty move together

BlueCap uses a controlled acquisition geometry rather than selecting an arbitrary value from a sensor range. The three settings below are designed as one system.

Terrain clearance35 m AGLChosen to maintain practical clearance above typical tropical and subtropical canopy while retaining useful sensitivity to near-surface radioelement contrast.
Cross-track geometry25 or 50 m linesThe client selects the production spacing for the required product. A 100 m option can be used in selected cases for draft mapping before a tighter survey is commissioned.
Along-track stability18 ±1 km/hThe production target, held relative to the terrain. The sensor maximum is 20 km/h, but maximum speed is not the survey target.
Why stability matters: at a 5 Hz record rate, 18 km/h is about one metre of travel per spectrum. Holding speed within ±1 km/h keeps along-track sampling and count exposure consistent instead of trading measurement quality for a small speed gain.
Before line-km

Inputs required to design the survey

Polygon, CRS and terrain

Area, relief, take-off sites, obstacles, exclusion zones and legal operating constraints define the feasible geometry.

Geological decision

The target model, expected dimensions and decision the map must support determine whether radiometric contrast is useful.

Existing evidence

Geological, geochemical, magnetic, LiDAR, DEM and previous radiometric data show the actual information gap.

Delivery and acceptance

Required K–eU–eTh products, resolution, raw data, formats, metadata and QC criteria are agreed before mobilisation.

From raw spectrum to reviewable maps

A radiometric delivery should not collapse source spectra into a few attractive rasters. Every mapped product must remain traceable to observation time, GNSS, detector state, flight geometry, correction parameters, spectral method, grid settings and the QC decisions applied to the project.

RAWSpectrum + GNSS + detector state
Retain source spectra, time, position, live/dead time and mission records.
01

Acquisition integrity

Review timing, GNSS, detector state, flight gaps, altitude, speed and spectral behaviour before accepting each sortie.

02

Detector and background

Check live/dead time, energy stability, background, drift and the calibration information applicable to the configuration.

03

Environmental effects

Consider altitude, air density, atmospheric radon, moisture and changing surface conditions where they affect comparability.

04

Spectral separation

Apply the agreed window analysis or Full Spectrum Analysis with calibration and stripping parameters preserved in the record.

05

Levelling and gridding

Generate consistent K, eU, eTh and total-count products without smoothing away narrow contrasts or concealing seams.

06

Technical review

Record software version, exceptions, acceptance criteria, reproducibility information and the limits of interpretation.

Project delivery

A mapped result plus the evidence needed to review it

K · eU · eTh · total count · ratios

Source and processed tables

Spectra, time, position, detector state and agreed corrected values in documented machine-readable formats such as JSON, NMEA or CSV where applicable.

Spatial products

K, eU, eTh, total-count and approved ratio grids, rasters, contours or vectors with CRS, datum, cell size, units and no-data definition.

QC and metadata

Processing record, calibration references, parameters, reflight notes, exceptions and interpretation cautions required for defensible reuse.

KpotassiumeUequivalent uraniumeThequivalent thorium

Useful near-surface evidence, not an orebody claim

Airborne gamma response is affected by distance to the surface, soil moisture, vegetation, cover, radon, terrain, material distribution and count statistics. Radiometric products become valuable when they answer a defined geological question and are checked against independent evidence.

Atmosphere / radonSoil · rock · regolithGamma response is dominated by near-surface material
01

Not a laboratory assay

Radiometric K, eU and eTh do not replace sampling, laboratory QA/QC, direct uranium chemistry or a geochemical model.

02

Not a universal depth detector

The signal is dominated by near-surface material; deep targets or targets beneath substantial cover may not create a direct surface signature.

03

Not immune to surface conditions

Moisture, transported cover, vegetation, sensor height and atmospheric radon can weaken or change the measured response.

04

Not a resource statement

An anomaly does not establish orebody geometry, grade, thickness, tonnage, a mineral resource or an ore reserve.

Independent evidence

Use each survey layer for the question it can answer

Project scoping

Start with the geological decision, not the sensor name

Send the polygon, CRS, target model, existing datasets, required K–eU–eTh products, resolution and schedule. BlueCap can then assess payload integration, acquisition geometry, count statistics, QC, processing and project fit.

Discuss the survey decision with BlueCap
Exploration compilation combining surface geochemistry, apparent-conductivity geophysics, mapped structures and drill-defined gold vein prospects with assay grades
How near-surface evidence is used in practice: surface geochemistry and geophysical anomalies vector towards targets, and drilling with laboratory assays carries the proof — the anomaly is the question, not the answer.

These are the acquisition parameters BlueCap uses to design and deliver the service. The client confirms the required line spacing and outputs before final route release; BlueCap controls the AGL setpoint, stable mapping speed, aircraft integration, field QC and processing workflow.

Calculate an indicative survey cost, schedule and mobilisation →

Project enquiry

BlueCap Starts with the Survey Decision

We use the Portal to turn your survey polygon into a quote-ready BlueCap project, review DEM-aware 2D and 3D mission design, follow field acquisition, and keep processing outputs and deliverables in one client workspace.

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.