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ERDI OEM LASER MODULE

LRF1525C 1.54 µm Rangefinder | ≥500 µJ Module, 15 km Large-Target Test

From $3,000 USD / unitLowest published unit price at 501+ pieces. Shipping included.
Product modelLRF1525C

LRF1525C is a 1.54 µm ±0.02 µm rangefinder with ≥500 µJ module energy and a 50 mm receiver lens. Its ≥15 km result applies to a 4 × 6 m target at 30% reflectance and visibility ≥18 km.

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MODEL-LEVEL DATA

Detailed LRF1525C Specifications

The technical material below is retained for this model only. Do not transfer a range, pulse, interface, mechanical or safety value from another 1535 nm product.

Specifications

LRF1525C is a 1535 nm pulsed distance-measurement module. Its assigned laser source is ER300; receiver-component data below come from the supplied APD-A13B001 R01 document. The three specification levels describe different assemblies and measurement conditions.

1. LRF1525C module specifications

Source clarifications

The source J30J interface table labels two supply contacts “VCC 5V” but describes their function as “12V Input Positive”. The conflicting source labels are retained for traceability, not as wiring instructions. Use the confirmed connector record supplied with the ordered unit.

LRF1525C — TECHNICAL SPECIFICATIONS
Project Performance Indicators
Model LRF1525C
Laser Wavelength 1.54μm±0.02μm
Module laser-safety statementClass I stated in the module document. Final accessible-emission classification applies to the complete configuration.
Divergence Angle ≤0.3 mrad
Laser Energy ≥500 μJ
Launch Lens Diameter Φ15 mm
Receiver Lens Diameter Φ50 mm
Measuring Range

(Reflectance 30%; visibility ≥ 18 km.)

4m×6m Objective ≥15 km
Minimum Range ≤50 m
Ranging Frequency 0.5Hz ~10Hz
Communication interface RS422
Ranging Accuracy ±2 m
Range Resolution ≤0.1m
Precision Rate ≥98%
False Alarm Rate ≤1%
Pin-in-lead package model J30J
Supply Voltage DC12 V
Standby power consumption ≤1.2W
Average power consumption ≤2 W
Peak Power Consumption ≤3W
Weight ≤400g
Dimension (L×W×H) 125mm×85mm×58.5mm
Operating Temperature -40~+70 ℃
Storage Temperature -55~+75 ℃
Impact Resistance Meet the MIL-STD-810G testing standard
Vibration Resistance Meet the MIL-STD-810G testing standard
LRF1525C — PIN INTERFACE

External plug-in XS3

Model:Molex51021-0500

Remark

1

TTL RX

3.3V

2

TTL TX

3.3V

3

CTRL

3.3V-5V power on, 0V power off

4

+12V

Power supply+

5

GND

Power supply-

LRF1525C — PIN INTERFACE

Pin

Definition

Function

Remarks

1

GND

Serial Port Ground

 

2

GND

12V Input Negative

 

3

GND

12V Input Negative

 

4

VCC 5V

12V Input Positive

 

5

VCC 5V

12V Input Positive

 

6

RS422 RX+

Serial Port Receive +

From the upper computer to the rangefinder

7

RS422 RX-

Serial Port Receive -

From the upper computer to the rangefinder

8

RS422 TX-

Serial Port Transmit -

From the rangefinder to the upper computer

9

RS422 TX+

Serial Port Transmit +

From the rangefinder to the upper computer

Model-specific mechanical and interface drawings

LRF1525C OUTLINE DIMENSION(mm) source drawing 1
LRF1525C: OUTLINE DIMENSION(mm). Original model-bound drawing.

2. ER300 source-laser specifications

ER300 standalone laser component
ParameterValue
Optical wavelength1535 nm
Pulse energy≥300 µJ
Optical pulse width5 ns
Drive pulse width≤2.4 ms
Repetition rate1–10 Hz
Pulse stability10% (definition/statistical method not stated)
Raw beam diameter0.3 mm
Initial beam divergence≤7 mrad
Transverse modeTEM00
Operating / storage temperature−40 to +65 °C / −55 to +75 °C
Package dimensions / mass25 × 8 × 6.8 mm / 8.5 g
Component electrical entry2 V, 12 A
Shock / vibration entries1500 G, 0.5 ms / 20–2000 Hz, 20 G
Stated service life>1 million shots; test conditions not supplied

The electrical entries describe the component drive, not the module supply input. Drive conditions and pulse-width definitions must follow the component document and the individual factory record. An optical pulse-width value is not a pump-drive duration.

3. APD-A13B001 receiver-component specifications

Small screens: swipe the table horizontally to read all measurement conditions.

Supplied APD200 document — component values and conditions
ParameterValueMeasurement condition / scope
Device / active diameterAPD-A13B001 R01 / 200 µmSupplied APD200 document, p1
Detector spectral response interval800–1700 nmDetector response; not the filter passband
Responsivity0.9 A/W minimum; 1.0 A/W typicalλ = 1550 nm; incident power = 1 µW; M = 1
Dark current8 nA typical; 50 nA maximumVR = VBR − 3 V; incident power = 0
Multiplication factorM ≥10 / M ≥30λ = 1550 nm; 1 µW; respectively VBR − 3 V / VBR − 1 V
−3 dB bandwidth0.6 GHz minimum; 1.25 GHz typicalM = 10; RL = 50 Ω
Breakdown voltage35–50 VReverse current = 10 µA; incident power = 0
Capacitance1.8 pF typical; 2.0 pF maximumVR = VBR − 3 V; f = 1 MHz
Breakdown temperature coefficient0.05 minimum / 0.11 typical / 0.15 maximum V/°CReverse current = 10 µA; dark; −55 to +85 °C
Operating / storage temperature−40 to +85 °C / −55 to +125 °CComponent absolute-maximum table; not module environmental ratings
Maximum biasVBRAbsolute maximum, not a recommended operating setpoint
Maximum forward / reverse current5 mA / 3 mAAbsolute maximum ratings, not continuous design targets
Filter centre wavelength1535 ±5 nmSupplied filter table, p3
Filter FWHM<37 nmFull width at half maximum
Transmission at centre wavelength>90%Filter specification, not total receiver throughput
Blocking specificationT <1%; source lists 400–1750 nmStop-band/transition edges are not numerically defined; the stated blocking span is not a guarantee at every wavelength.
Optical surface quality60/40Source label: surface quality; not a transmission value

Responsivity is measured at 1550 nm; a value measured there is not silently relabeled as a measured 1535 nm value. Absolute maxima are stress limits. The filter document includes an illustrative spectrum, but does not define numerical transition edges or off-axis performance. No additional spectral guarantee is inferred.

SOURCE CONDITIONS

Model-specific conditions and limits

Conditions are retained only when the source states them. They are not reconstructed from a nominal range or wavelength.

Operating conditions

Read a range value together with its test case

Target dimensions, surface reflectance and atmospheric visibility are part of the range specification. The beam may partly miss a small object, illuminate a sloped surface or return from several depths. A high-reflectance building result cannot establish the same distance to a smaller or darker object. Humidity and temperature conditions shown in a source table describe that test; visibility is not interchangeable with a guaranteed transmission percentage.

Measurement rate and electrical conditions

Measurement rate is the number of reported measurement opportunities per second. It is separate from optical pulse duration, receiver bandwidth and the time required for an individual return. Read operating power at the frequency and supply printed beside it. Peak power describes a different electrical requirement from average power; an average figure alone does not characterize supply transients.

Environmental and measurement context

A module temperature rating, laser-component temperature range and APD maximum rating describe different assemblies. Likewise, a named vibration standard does not disclose every method, mounting condition or acceptance threshold. Range repeatability, reported resolution and absolute accuracy are different quantities: a fine numerical display increment does not establish the error of the complete measurement.

HOW TO READ THE MEASUREMENT

Pulsed Time-of-Flight Ranging

Technical principle

A pulse, a return and a measured interval

Pulsed time-of-flight ranging measures elapsed time between an optical launch reference and a detected echo. The basic relationship is R = vΔt/2, where v is the speed of light in the propagation medium. The factor of two accounts for the outward and return journeys. The familiar expression using c treats propagation as approximately in air/vacuum; absolute metrology also considers refractive index and calibrated internal delays.

The measurement chain contains a pulsed source, transmit optics, an illuminated surface, collection optics, spectral filtering, a detector and timing electronics. ER300 supplies optical pulses. The module's output beam is described by its own optical specification after integration. A nanosecond laser pulse is not the same quantity as a millisecond pump-drive pulse or a hertz measurement rate.

Initial divergence and the integrated beam

A bare source has its own beam diameter and divergence. Collimating and expanding optics alter the relationship between beam size and angular spread. Therefore the component's initial divergence and the assembled module's transmitter divergence belong in separate rows. Finite beams still diffract, and real optics add aberrations, alignment error and clipping. A quoted angular value also needs a full-angle/half-angle convention and a beam-width definition before it supports a numerical footprint calculation. Those definitions are not invented where the product record omits them. Newport's optics explanation provides the general context.

Why the same laser can appear in different range classes

The laser source is one contributor to system performance. At a fixed, uniform irradiance at the receiver entrance, a circular unobscured collecting aperture has area A = πD²/4. With equal throughput and no clipping, collected optical power is proportional to that area. A larger receiver lens can therefore collect more of the available return. This is an area relationship under stated assumptions, not a range multiplier and not a test result for this product.

The return reaching that aperture also depends on transmitted energy, beam spread, object size and reflectance, surface orientation, atmospheric attenuation and optical transmission. Increasing collection area may collect additional background light as well. Receiver field of view, throughput, detector response and the decision process determine how much useful information remains. Consequently, models sharing ER300 can have different conditional range specifications, and their ranges should be compared using equivalent target and weather conditions.

APD conversion, filtering and timing

The supplied InGaAs APD generates photocurrent and provides internal avalanche multiplication. Its responsivity at M = 1 describes conversion before multiplication; the gain values describe a specified reverse-bias condition. Internal gain accompanies multiplication noise. Dark current, capacitance and bandwidth also matter, so the maximum tabulated gain is not automatically the best operating point. The specified gain conditions below breakdown describe linear APD operation, not evidence of single-photon Geiger-mode operation. Hamamatsu's detector guide explains these distinctions.

The narrowband filter transmits the useful wavelength region while rejecting specified out-of-band light. It does not reject background that lies inside its passband. Its centre transmission is not the throughput of the lens, window, filter and detector assembly together. A detector bandwidth measured at 50 Ω likewise does not specify the installed amplifier bandwidth or the finished rangefinder's accuracy.

Short distances, long distances and processing

At short distances, the return arrives near the launch event; optical overlap, prompt scatter and receiver recovery can limit the usable minimum distance. A strong close return can also exceed the linear region. At long distances, reduced return strength makes background, noise and signal discrimination more significant. These are different mechanisms, so good long-range performance does not imply a zero blind zone or a guaranteed result at every shorter distance.

In a threshold-based timing receiver, changes in pulse amplitude can shift the threshold-crossing time, called time walk. Calibration, multiple-return discrimination and signal estimation are general approaches discussed in the literature. Signal estimation and timing correction depend on the receiver architecture; no specific firmware method is claimed without a model-specific record. Reported multi-target capability alone does not disclose the underlying algorithm. Kurtti, Jansson and Kostamovaara examine receiver/TDC timing behavior in their own research hardware.

Pulse energy describes emitted energy per pulse; its effect cannot be separated from pulse width, divergence, optical losses, receiver threshold and the stated target/atmosphere conditions. It is not a substitute for a model-specific near- or long-range acceptance test.

APPLICATION REVIEW

Source-stated application context

Application labels indicate evaluation context, not automatic fitness for a finished system.

This model’s larger receiver aperture and defined large-target case provide concrete selection differences from the 40 mm-receiver 10 km and 12 km records. Its transmitter lens is 15 mm, with ≤0.3 mrad divergence. No new range value is calculated from that aperture or energy; the controlled target-condition table remains the performance reference.

The module lists DC 12 V supply, RS-422 communication, 0.5–10 Hz ranging, a 125 × 85 × 58.5 mm envelope and ≤400 g mass. Its ≥500 µJ module-energy row is kept separate from the named ER300 component table. The two specification levels are not silently reconciled by replacing one number with the other.

INTEGRATION CHECK

Confirm short- and long-distance acceptance conditions

  • Define minimum distance, target material, reflectance, size and incidence angle.
  • Check receiver recovery, optical-axis overlap and strong-return handling at the intended near limit.
  • Verify supply tolerance, peak current, grounding, interface levels, connector and timing with the ordered revision.
  • For long-distance acceptance, state target geometry, visibility, weather, background and required detection probability.
  • Test with the installed window, boresight, field of view, enclosure and thermal path rather than a bare module alone.
  • Evaluate accessible emission, labels and failure conditions again for the finished laser product under IEC 60825-1.
TECHNICAL FAQ

Questions to resolve before design release

Which target is used for the 15 km figure?

The LRF1525C record specifies ≥15 km for a 4 × 6 m target at 30% reflectance and visibility ≥18 km. This large-target test does not establish the same distance to a human-size object or a smaller reference panel. Keep the target and atmosphere attached to the claim.

Is the advertised 500 µJ value the ER300 component rating?

No. The ≥500 µJ entry is in the LRF1525C module table. ER300 is separately identified in the component section with its own specification. This page preserves both source levels and does not overwrite the module energy with the standalone component’s value or claim an undocumented conversion between them.

What aperture differences distinguish LRF1525C?

Its optical table lists a 15 mm transmitter lens and a 50 mm receiver lens, with ≤0.3 mrad divergence. These differ from the 40 mm receivers in several other long-range C-series records. Aperture alone is not a demonstrated multiplier for distance performance or a substitute for the specified target test.

What does the 0.5–10 Hz entry describe?

It describes the module’s ranging frequency, not optical pulse duration or an independently measured update guarantee for every return condition. The module also lists RS-422 and DC 12 V supply. Use the ordered version’s operating conditions when assessing its reporting behavior in a larger system.

Which package and power figures can be used for comparison?

The record lists 125 × 85 × 58.5 mm, ≤400 g mass, ≤2 W average power and ≤3 W peak power. These are module-level values, distinct from source-laser drive conditions. Mechanical size or average power should not be used to infer a new target-range capability.

ENGINEERING REFERENCES

Product evidence and general technical context

The model PDF controls model claims. Public references below explain general engineering principles only.

  1. LRF1525C controlled module datasheetThe module-specific parameters, target conditions and version notes cited on this page.
  2. Practical application of pulsed “eye-safe” microchip laser to laser rangefindersGeneral context for pulsed 1535 nm rangefinder architecture and source/receiver selection.
  3. Light Transmission in Fog: The Influence of Wavelength on the Extinction CoefficientWhy atmospheric conditions must remain attached to a stated ranging test case.
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