200M 400M 200M
RNG: 2.4 KM
BRG: 047°
ALT: 3,200 FT
SPD: 480 KTS
HDG: 012° N
TGT: ALPHA-7
MODE: SEARCH
PWR: NOMINAL
FREQ: X-BAND
STATUS: LOCK
NAVTGTWPNDEFRDRCOM
MIL-STD-1553IFF: ACTIVELINK-16: SYNC
SECTOR: ALPHA
THREAT: CLEAR
RADAR: ACTIVE
TRACK: 6 TGT
LAT 28.6213°N LON 77.3873°E
NX
Neometrix Target Acquired
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NMX‑PTR‑DTSN82 / Rev 01 / ATF · NAS 1638 Cl‑4 · 150,000 LPH · 1000 RPM / Aircraft Fuel Injection System Noida · India · 2026
NMX-PTR-DTSN82

ATF fuel pump test rig.

Precision running-in and performance testing of the centrifugal fuel booster pump DTSN-82 — part of the aircraft fuel injection system — at varied inlet absolute pressure, delivered flow, and drive RPM using Aviation Turbine Fuel.

ATF Fuel Pump Test Rig DTSN-82 — Neometrix, Noida
Fig · 01 Pump test rig DTSN-82 — ATF circuit with pressure & flow measurement
Max Flow
150kLPH
Inlet Pressure
3.2kg/cm²
Fluid Temp
120°C max
Drive Speed
1000RPM
Cleanliness
NAS 1638Cl-4
01
Overview

Running-in and testing the DTSN-82 booster pump.

Complete ATF-circuit test rig for performance qualification of the centrifugal fuel booster pump at the heart of aircraft fuel injection systems.

ATF Pump Test Rig DTSN-82 — ATF circuit detail
Fig · 02 ATF circuit — inlet pressure control, flow measurement, thermal management

The ATF Fuel Pump Test Rig DTSN-82 is purpose-built for running-in and functional testing of the centrifugal fuel booster pump DTSN-82, which is a critical component of the fuel injection system in military and civil aircraft.

The rig creates controlled test conditions by pressurising the ATF tank using shop air and a vacuum pump, achieving inlet absolute pressures from 0.2 to 3.2 kg/cm² at the unit under test (UUT). Delivered flow is measured over the full operating range of 500 to 150,000 LPH at varied drive shaft RPM up to 1000.

ATF fluid cleanliness held to NAS 1638 Class-4 throughout the test cycle.

A circulating water cooling system maintains the working fluid within the permissible temperature envelope of 20 to 120°C. All wiring is heat- and moisture-resistant, coded, and routed through cable trays per IS norms. Emergency shutdown and drive interlocks are standard.

02
Key Features

Built for ATF environments.

Four core engineering disciplines that define the DTSN-82 test rig.

Feature · 01

ATF-Grade Wiring & Routing

All interconnect wiring is heat-resistant and moisture-resistant by specification. Wires are properly coded, bunched, and routed through dedicated cable trays in compliance with IS norms — critical in an ATF vapour environment.

Heat-Resistant · IS Norms · Cable Tray Routing
Feature · 02

Leak-Proof Assembly

All individual components are leak-tested before assembly. The complete final assembly undergoes a further leak test under operating pressure — essential when working with aviation turbine fuel at pressures up to 3.2 kg/cm².

Component Leak Test · System Leak Test · ATF Tight
Feature · 03

Safety Interlocks & Emergency Shutdown

Emergency shutdown is hard-wired and independent of the control system. Drive interlocks prevent the pump from being started unless all pre-conditions (fluid level, temperature, cleanliness monitoring) are met — protecting both the UUT and the operator.

E-Stop · Drive Interlock · Independent Safety Circuit
Feature · 04

Industrial Finish & Aesthetic

Panels are painted in a suitable colour with a mat finish. All structural elements and fluid components are painted in a coordinated colour scheme — presenting a professional, inspection-ready appearance for defence and aerospace customer environments.

Mat Finish · Coordinated Colour Scheme · Defence-Grade
03
Image Gallery

The rig, two views.

ATF circuit overview and pump mounting detail.

Fig · 03 2-view photo documentation · Pump Test Rig DTSN-82 · Neometrix Noida
04
Specifications

Full system parameters.

Standard NMX-PTR-DTSN82 configuration. Custom pressure ranges, flow instrumentation, and control configurations available on request.

System ReferenceATF Fuel Pump Test Rig DTSN-82  ·  NMX-PTR-DTSN82
Working FluidAviation Turbine Fuel (ATF)
Fluid Density at 20°C0.78 gm/cm²
Fluid CleanlinessBetter than NAS 1638 Class-4
Inlet Absolute Pressure (UUT)0.2 to 3.2 kg/cm²
ATF Tank Pressure Range−1 to 3.2 kg/cm² (via shop air & vacuum pump)
Permissible Fluid Temperature20 to 120°C
Flow Through UUT500 to 150,000 LPH
Cooling MediumCirculating water
Drive Shaft Speed (Running-in)Up to 1000 RPM
Power Supply415V ±10%  ·  3-phase  ·  50 ±2 Hz
Wiring StandardHeat- & moisture-resistant, coded, IS norms, cable tray routed
SafetyEmergency shutdown  ·  Drive interlocks
05
Applications

Where it is used.

Aircraft fuel system component manufacturers, MRO facilities, and defence overhaul depots requiring certified pump performance data.

A · 01Running-in of centrifugal fuel booster pump DTSN-82 after manufacture or overhaul
A · 02Performance testing at varied inlet absolute pressure (0.2–3.2 kg/cm²) and drive RPM
A · 03Delivered flow verification across the full range (500–150,000 LPH) at specified pressure
A · 04Qualification testing for aircraft fuel injection system components — defence and civil aviation
A · 05MRO acceptance testing of pump after repair — verifying return-to-spec before re-installation
A · 06R&D performance mapping of pump across pressure-flow-RPM operating envelope
06
In Depth

The complete technical read.

Engineering narrative for test and MRO engineers specifying a centrifugal fuel pump test rig.

01 — The UUT

The DTSN-82 centrifugal fuel booster pump

The DTSN-82 is a centrifugal fuel booster pump forming a critical part of the fuel injection system on certain military aircraft. Its role is to maintain positive fuel pressure at the inlet of downstream fuel injection components across the flight envelope — from sea-level ground operation to altitude conditions where fuel tank pressure may drop below ambient.

02 — ATF Circuit

ATF pressure and temperature control

Shop air and a vacuum pump pressurise or depressurise the ATF tank to set the absolute inlet pressure at the UUT — from as low as 0.2 kg/cm² (simulating altitude cavitation margin) to 3.2 kg/cm² (boosted ground conditions). A circulating water heat exchanger controls the ATF temperature throughout the test window of 20 to 120°C.

03 — Cleanliness

NAS 1638 Class-4 fluid cleanliness

Aviation fuel system components are sensitive to particulate contamination. The rig maintains ATF cleanliness better than NAS 1638 Class-4 throughout the test cycle using appropriate filtration in the recirculation circuit. This protects the precision clearances inside the UUT and ensures test results are not corrupted by contamination-induced wear during the running-in phase.

04 — Safety

ATF safety — shutdown and interlocks

Aviation turbine fuel is flammable. The rig's safety architecture includes a hard-wired emergency shutdown independent of the control PLC, interlock chains on all drives that prevent start unless fluid conditions are confirmed, and heat- and moisture-resistant IS-compliant wiring throughout. Component-level and final assembly leak tests are conducted under ATF before commissioning.

07
FAQ

Common questions.

Q · 01What pump does this rig test?
The rig is designed for the centrifugal fuel booster pump DTSN-82, which is part of the aircraft fuel injection system. It can be adapted for similar centrifugal fuel pumps on request.
Q · 02What fluid does the rig use?
Aviation Turbine Fuel (ATF) with density 0.78 gm/cm² at 20°C, maintained at NAS 1638 Class-4 cleanliness or better throughout the test cycle.
Q · 03What inlet pressure range can the rig achieve?
Absolute pressure at the UUT inlet ranges from 0.2 to 3.2 kg/cm². The ATF tank pressure can be set from -1 to 3.2 kg/cm² using shop air and a vacuum pump.
Q · 04What safety features are included?
Emergency shutdown hard-wired independent of the control system, drive interlocks, IS-compliant heat- and moisture-resistant wiring, component-level leak testing, and final assembly leak testing under ATF.
Q · 05What power supply is required?
415V ±10%, 3-phase, 50 ±2 Hz.
Q · 06What after-sales support does Neometrix provide?
Installation, commissioning, operator training, preventive maintenance, and on-site service. Standard 12-month warranty with optional annual maintenance contracts.
08
Downloads

Technical documents.

09
Presentation

Product overview deck.

Seven-slide summary of the NMX-PTR-DTSN82 — purpose, ATF circuit, specifications, features, and applications.

NMX‑PTR‑DTSN82  ·  Rev 01

ATF Fuel Pump
Test Rig DTSN-82

Centrifugal Fuel Booster Pump  ·  Aircraft Fuel Injection System  ·  150,000 LPH

Neometrix Engineering Pvt Ltd  ·  Noida, India

ATF Fuel Pump Test Rig DTSN-82
02 / 07

What it tests

Purpose-built for running-in and performance testing of the centrifugal fuel booster pump DTSN-82 — part of the fuel injection system of aircraft. Tests at different inlet absolute pressures and delivered flow at varied drive shaft RPM.

The UUT
Centrifugal fuel booster pump DTSN-82 — aircraft fuel injection system component
Test Objective
Running-in after manufacture or overhaul; performance mapping across pressure-flow-RPM envelope
Working Fluid
Aviation Turbine Fuel (ATF) · 0.78 gm/cm² at 20°C · NAS 1638 Class-4
03 / 07

ATF Circuit Architecture

Pressurised ATF tank (shop air + vacuum pump) sets absolute inlet pressure at UUT. Circulating water heat exchanger controls fluid temperature. NAS 1638 Class-4 filtration in recirculation loop.

Inlet Pressure Control
Shop air + vacuum pump sets ATF tank pressure from -1 to 3.2 kg/cm² → absolute inlet at UUT 0.2–3.2 kg/cm²
Temperature Control
Circulating water heat exchanger maintains ATF at 20–120°C throughout the test cycle
04 / 07

Key Specifications

150kLPH
Max Flow (UUT)
3.2kg/cm²
Max Inlet Pressure
120°C
Max Fluid Temp
1000RPM
Drive Shaft Speed
NAS Cl-4
Cleanliness
415V
Power Supply
Flow range: 500–150,000 LPH  ·  Density: 0.78 gm/cm² at 20°C  ·  Cooling: circulating water
05 / 07

Four Core Engineering Features

Wiring
Heat- & moisture-resistant, coded, routed per IS norms in cable trays — safe in ATF vapour environment
Leak Proof
Component-level and final assembly leak test under ATF at operating pressure before commissioning
Safety
Hard-wired E-stop independent of control system  ·  drive interlocks on all motors
Designed for ATF environments — defence and civil aviation MRO.
06 / 07

Applications

  • Running-in of DTSN-82 pump after manufacture or overhaul
  • Performance testing at varied inlet pressure (0.2–3.2 kg/cm²) and RPM
  • Flow verification across 500–150,000 LPH range at specified pressure
  • Qualification testing for aircraft fuel injection system components
  • MRO acceptance testing after pump repair — verifying return-to-spec
  • R&D performance mapping across pressure-flow-RPM operating envelope
07 / 07

Ready to specify?

Tell us your pump model, required pressure-flow test points, fluid type, and cleanliness specification. We design the rig around your qualification requirements.

Neometrix Engineering Pvt Ltd  ·  Noida, India  ·  neometrixgroup.com
1 / 7
Related

Other test systems from Neometrix.

Get a proposal

Tell us your pump model
and test specification.

We design the ATF circuit, specify instrumentation, define cleanliness and safety requirements, and commission the rig at your facility.

Request proposal +91 7777 876 876

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Engineered To Standards Used In UK, NATO & U.S. Defence Procurement
DEF STAN (UK MoD)
NATO STANAG
RTCA/EUROCAE DO-160
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