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‑JST‑30 / Rev 00 / ground support / air start · flight line 2026 · Product Page
NMX-JST-30 · ENGINEERED TO ORDER — JET AIR STARTER TROLLEY

Not pressure. Flow that will not sag.

Shop air is high pressure at low flow. A starter cart is the opposite — modest pressure at very large mass flow — which is why a cart quoted on pressure alone tells you nothing about whether it can start anything. And the demand moves: as the air turbine starter spins up, speed, back-pressure and flow all change together, so delivery has to hold through the whole sequence. Let it sag halfway and the engine can hang below self-sustaining speed while fuel burns, or run hot — both engine-damage events. A start that stalls halfway is worse than a start never attempted. So we size for the hot-and-high day, not the brochure day, and we quote starts per hour, not a start. No delivered starter trolley is claimed.

Illustrative image, not a delivered system — a towable ground support trolley standing alone on an empty concrete apron: an enclosed pale grey acoustic cabinet on a low four-wheel chassis, a long steel drawbar with a tow eye resting on the ground, a vertical exhaust stack with a rain cap at the rear, large louvred intake panels along the side, a thick coiled grey flexible duct hose stowed in a steel cradle, rubber chocks at the wheels, overcast daylight on wet concrete, no aircraft, no people and no markings
Fig · 01 The cart, chocked and stowed — drawbar down, hose in its cradle, ready for the next launch — illustrative, not a delivered system
The rating
mass flowheld at pressure
Sized for
hot & highnot the easy day
Duty
starts per hournot “a start”
Air
dry & filteredit enters the engine
Lets go at
self-sustainingjob done
ISO 9001 / 14001 Engineered to order Flight-line cart franchise Performance-tested Noida · India
01
Overview

A flow source that happens to be portable.

Almost every mistake in specifying one of these comes from thinking of it as a compressor on wheels. It is not. Its output is judged the way a pump's is — by how much it moves, sustained, against the back-pressure it actually meets — and everything from the prime mover choice to the hose diameter follows from that.

Illustrative image, not a delivered system — close view of the delivery end of a large-bore flexible air duct on a concrete apron: a thick grey reinforced hose about the diameter of a dinner plate curving across the frame and ending in a plain machined aluminium bayonet-style coupling with a hinged blank dust cap standing open on its pin, a shallow galvanised steel cradle behind it, damp apron with shallow puddles, flat grey daylight, no markings
Fig · 02 The end that matters — large-bore, heavy, hot after a start, and its own volume fills before the aircraft sees flow — illustrative, not a delivered system

The rating is flow held at pressure. Delivery pressure for engine starting is modest — a few bar, not the hundreds a charging system works at — but the mass flow is large and has to be sustained for the whole crank. A supplier who leads with pressure is answering an easier question than the one that matters. The right specification names flow, at a stated delivery pressure, at a stated ambient, and says how long it can be held.

The demand is a moving target. As the starter spins up, the turbine passes more air and the back-pressure changes with it, so the operating point walks across the map during a single start. A cart with a steep characteristic can meet the initial demand and then fall away precisely as the engine approaches light-up — the worst possible moment. That is the origin of the hung start: the engine stops accelerating, fuel keeps burning, and temperatures climb where there is not yet enough airflow to carry the heat away.

And the worst day is the normal day. A turbine or compressor loses output as it gets hotter and as the air gets thinner, so output falls on exactly the days the engine is hardest to start. Sizing against a temperate sea-level figure produces a cart that demonstrates beautifully and disappoints in service. Specify the derated output at the worst airfield and ambient the fleet actually operates from, and treat the headline number as marketing.

We build the trolley, the whole air path, the hose management and the controls, and we performance-test it. The prime mover and the compressor are bought in certified. The aircraft's own air turbine starter and engine are not ours.
Sustained

Flow, all the way through

Held across the whole crank, not just at the moment the valve opens — the sag is the failure.

Derated

Quoted at your worst day

Output stated hot and high, where the engine needs most and the cart gives least.

Repeatable

Starts per hour

Consecutive launches without a long cool-down — duty cycle is the honest capability.

02
Architecture

Connect, crank, let go.

The schematic follows the start — connecting through the hose, spinning the air turbine starter, holding the flow through the sequence, and releasing the moment the engine is self-sustaining — then shows the machine beneath it: prime mover and compressor, filtration and water separation, the duct and coupling, and the control and protection that allows a clean abort.

FIG · 03AIR START ARCHITECTURE · PRIME MOVER + COMPRESSOR / FILTER + WATER / DUCT, HOSE & COUPLING / CONTROL & PROTECTION
CONNECT → SPIN THE STARTER → HOLD THE FLOW → RELEASE AT SELF-SUSTAINING A FLOW SOURCE, NOT A COMPRESSOR - SHOP AIR IS HIGH PRESSURE AND LOW FLOW. THIS IS THE OPPOSITE, SO A CART QUOTED ON PRESSURE ALONE SAYS NOTHING ABOUT WHAT IT CAN START. THE RATING MASS FLOW HELD AT DELIVERY PRESSURE SIZED FOR THE HOT AND HIGH DAY, NOT THE BROCHURE DAY CONNECT THE HOSE VOLUME FILLS BEFORE THE AIRCRAFT DOES SPIN THE STARTER THE AIR TURBINE CRANKS TOWARD LIGHT-UP HOLD THE FLOW DEMAND CHANGES ALL THE WAY THROUGH RELEASE AT SELF-SUSTAINING SPEED - JOB DONE IF DELIVERY SAGS MID-CYCLE THE ENGINE CAN HANG BELOW SELF-SUSTAINING SPEED WHILE FUEL BURNS - A START THAT STALLS HALFWAY IS WORSE THAN NO START AT ALL PRIME MOVER + COMPRESSOR TURBINE FOR FLOW, OR DIESEL AND SCREW FILTER + WATER IT GOES THROUGH THE STARTER, THEN THE ENGINE DUCT, HOSE + COUPLING HEAVY, HOT, AND ONE PERSON MUST WORK IT CONTROL + PROTECT CLEAN ABORT, AND A RECORD THAT LASTS OUR ROLE: TROLLEY + RUNNING GEAR, THE WHOLE AIR PATH, HOSE MANAGEMENT + GROUND CONNECTOR, CONTROLS + PROTECTION, ACOUSTIC ENCLOSURE, PERFORMANCE TEST + AMC DETAIL · WHAT THE BROCHURE FIGURE HIDES AMBIENT HOT AND HIGH TAKES OUTPUT HOSE LOSSES RATED AT THE CART, NOT THE JET DUTY CYCLE ASK STARTS PER HOUR, NOT A START GOAL: FLOW AT THE AIRCRAFT ON THE WORST DAY IT WILL SEE COMBINATION CARTS ADD ELECTRICAL POWER AND CONDITIONED AIR - CONVENIENT, BUT ONE FAILURE THEN GROUNDS THREE SERVICES. MAKE THAT TRADE DELIBERATELY. DELIVER FLOW, NOT PRESSURE SUSTAIN THE WHOLE SEQUENCE REPEAT START AFTER START
Fig · 03 Flow at the aircraft, on the worst day it will see
Arc · 01

Prime Mover & Compressor

Gas turbine with load compressor for flow in a compact package, or diesel with a screw compressor for running cost and simplicity.

Arc · 02

Filtration & Water Separation

This air goes through the starter and then the engine, so moisture, oil carry-over and particulate are all specified out.

Arc · 03

Duct, Hose & Coupling

Large-bore ducting, cradles or reelers and the ground connector — sized for pressure drop, and for one person to handle.

Arc · 04

Control & Protection

Start sequencing, overspeed, over-temperature and low-oil-pressure trips, automatic shutdown and a clean abort.

Specifying or replacing flight-line start equipment? Send the engine's start-air demand, the airfield elevation and design ambient, and the sortie rate — a clause-by-clause compliance matrix within two working days · [email protected]
Send tender spec
03
Specifications

Reference cart, built to the fleet.

The parameters below describe a reference cart. Flow, delivery pressure, prime-mover choice, duty cycle, hose size and enclosure all follow from three givens: the engine's start-air demand, the airfield elevation and design ambient, and how many aircraft have to be launched in sequence.

Illustrative image, not a delivered system — the side doors of a ground support equipment cabinet standing open in a clean workshop: a compact turbine and compressor module on four rubber anti-vibration mounts on the base frame, a wide-bore duct elbow leaving the compressor into a horizontal cylindrical silencer, a tall pleated filter housing alongside with a plain blank-faced indicator on its head, neatly loomed wiring running to a plain grey control box with a blank front panel, painted steel floor plate, even workshop lighting, no people and no markings
Fig · 04 Inside the enclosure — module on isolators, duct into the silencer, filtration before anything reaches the hose — illustrative, not a delivered system

Where air start units go wrong

Quoted on pressure, with mass flow at that pressure left vague or stated only at an ideal ambient. Sized on a temperate sea-level day, then derated into uselessness at the hot, high airfield that generated the requirement. A single-start duty cycle sold to a flight line that has to launch a formation. Moisture and oil carry-over allowed into the delivery path, on air that ends up inside the engine. Hose volume and pressure drop ignored, so the number measured at the cart never arrives at the aircraft. Hose handling as an afterthought — too heavy, no cradle, impossible for one person in wind and rain. Noise treated as somebody else's problem next to a maintenance line. No clean abort, so an operator who sees something wrong has no safe way to stop. Combination carts adopted without the redundancy conversation. And records that stop at handover, when flow-at-pressure is exactly what drifts as a machine ages.

So the discipline runs the other way. Performance is stated as flow at delivery pressure at a named ambient and elevation, and measured that way at test. Duty cycle is proven by consecutive starts, not a single demonstration. Filtration and water separation sit in the delivery path as specification items. Hose bore, length and routing are chosen with the pressure drop calculated and the rating quoted at the coupling, not at the machine. Hose stowage is designed for one person. Acoustic treatment is specified where the cart will actually stand. Protection trips are real and testable, and the abort is clean. And the cart is handed over with a performance record that can be repeated later to show what it still does.

Full specification — expand
SystemJet air starter trolley / ground air start unit — prime mover, compressor, air path, hose management, controls & protection on a towable chassis
Governing IdeaA flow source, not a compressor — modest pressure at very large mass flow, the opposite of shop air
The RatingMass flow HELD AT delivery pressure, stated at a named ambient temperature and field elevation — not a headline pressure
Delivered ToThe aircraft's air turbine starter, cranking the engine to the speed at which fuel is introduced and the engine becomes self-sustaining
The Failure ModeHung start — delivery sags, the engine stops accelerating below self-sustaining speed while fuel burns; or a hot start. Both damage engines
Sizing CaseHot and high — prime mover and compressor both derate as ambient and elevation rise, exactly when the engine needs more air
Prime MoverGas turbine + load compressor (very high flow, compact, light) or diesel + screw compressor (lower running cost, simpler maintenance, larger and heavier)
Air QualityFiltration and water separation in the delivery path; oil carry-over prevented from reaching the aircraft
Duty CycleConsecutive starts without extended cool-down — set by oil and exhaust-gas temperature limits, cooling airflow and recovery time. Specify starts per hour
Hose & CouplingLarge-bore flexible ducting with cradle or reeler and a ground connector; pressure drop calculated and the rating quoted AT THE COUPLING; hose volume fills before the aircraft sees flow
Chassis & MobilityTowable at flight-line speed, drawbar and tow eye, brakes, chocks and wind tie-down, FOD-conscious detailing
EnclosureWeatherproof and acoustically treated — turbine-driven carts are loud, and they stand where people work
Control & ProtectionStart sequencing; overspeed, over-temperature and low-oil-pressure trips with automatic shutdown; clean abort; operator interface usable in gloves and rain
Combination UnitsAir + electrical power + conditioned air in one cart is possible — but one failure then grounds three services, and that trade is made deliberately
TestingFlow at delivery pressure, hot-day derate, consecutive-start duty, protection-trip proving — recorded and repeatable through life
Scope BoundaryOurs: trolley & running gear, complete air path (ducting, valves, filtration, water separation, silencing), hose management & connector interface, controls, protection, instrumentation, enclosure, assembly, performance testing, commissioning, documentation, training, spares & AMC. Bought-in certified: prime mover, compressor, filter elements, transducers, wheels & braking. Not ours: the aircraft's air turbine starter and engine
The FamilyBeside the delivered flight-line cart work, the HP air installations and the ground electrical power line — the same apron, a different service
StatusEngineered to order · quoted across jet air starter, portable engine-starting unit & starting-trolley requirements · no delivered starter trolley is claimed on this page
04
Variants

One service, four builds.

What changes is how the air is made, how much of it is needed, and whether the aircraft starts on air at all.

Var · 01

Turbine-Driven Air Start Trolleys

Gas turbine and load compressor — the high-flow, compact answer where sortie rate and hot-and-high performance dominate.

Var · 02

Diesel Screw-Compressor Units

Lower running cost and simpler maintenance — heavier and larger, but easier to keep serviceable away from a main base.

Var · 03

Portable Engine-Starting Units

Smaller aircraft and helicopters — compact starting trolleys and power packs where full air-start flow is not required.

Var · 04

Overhaul, Re-Power & AMC

Re-powering ageing carts, replacing the air path, re-instrumenting and re-proving flow at pressure — plus support.

05
Applications

Wherever an engine has to turn first.

Flight lines, hangars, test bays and the places with none of those.

A · 01Fast-jet flight lines & dispersals
A · 02Transport & helicopter fleets
A · 03Maintenance hangars & post-overhaul ground runs
A · 04Engine test bays needing start air
A · 05Forward & austere operating locations
A · 06Civil apron & MRO operations
06
FAQ

Common questions.

Plain-language answers from the engineering team.

Q · 01 Why does an aircraft need a cart at all — can it not start itself?
Some can and some cannot, and the difference decides whether this equipment is on the apron. A gas turbine cannot start unaided: it has to be turned to a speed where the compressor is delivering enough air for combustion to be self-sustaining, and only then can fuel be introduced and the engine take over. Something has to supply that cranking energy. Many transport and civil aircraft carry an auxiliary power unit which provides it internally, so they are independent on a normal day — but not when the auxiliary unit is unserviceable, which is exactly when a ground cart saves a sortie. Many other aircraft, particularly compact ones where there is no room or weight budget for an auxiliary unit, depend on ground equipment every single time. Where the engine has an air turbine starter, the cart supplies air. Where the aircraft starts electrically, the ground supply is direct-current power instead. Either way the ground equipment is not a convenience but part of the aircraft's dispatch chain, which is why availability, duty cycle and hot-day performance matter far more than they would for ordinary workshop plant.
Q · 02 Why is flow the specification rather than pressure?
Because the device at the other end is a turbine, and a turbine is driven by the mass of air passing through it, not by the pressure standing behind it. Delivery pressure for engine starting is modest — a few bar — and getting there is trivially easy; what is hard is sustaining a very large mass flow at that pressure for the length of a crank. So a cart advertised by pressure has answered the easy half of the question. The specification that means something is mass flow at a stated delivery pressure, at a stated ambient temperature and field elevation, sustained for a stated duration, and ideally measured at the coupling rather than at the machine. This is also why comparisons with workshop compressors mislead: a shop machine may make ten times the pressure and a small fraction of the flow, and would not turn a starter at all. It is closer to think of the cart as a very large fan with a pressure rise than as a compressor — the useful currency is throughput, and the pressure is only there to push it through the starter and the hose.
Q · 03 What is a hung start, and how does the cart cause one?
A hung start is an engine that lights but then stops accelerating, sitting stubbornly below self-sustaining speed with fuel burning. It is a genuinely bad place to be: the engine is producing heat but not yet enough airflow to carry that heat away, so exhaust-gas temperature climbs while the engine goes nowhere, and the crew has to shut down before limits are exceeded. The cart's contribution is straightforward. Cranking assistance must continue past light-up, through the region where the engine is producing some power but not enough to accelerate itself. If air delivery sags in that window — because the cart was marginal, because it was hot, because the hose was long, or because a previous start left it heat-soaked — the engine loses the help it still needs and hangs. Which is why a cart that produces a splendid figure at the start of delivery and then droops is worse than a smaller one that holds. It is also why duty cycle matters as a safety property and not just a productivity one: the second and third starts of a launch are the ones where a marginal cart has warmed up and quietly lost output.
Q · 04 Turbine or diesel — which should we buy?
It depends on your sortie rate and on who maintains the cart, and anyone who answers without asking those has not understood the question. A gas turbine driving a load compressor gives an enormous mass flow from a package light and compact enough to be towed easily and manoeuvred by hand. It starts quickly, it copes with consecutive launches well, and where flow is the binding constraint it is usually the honest answer. Against that it is thirsty, it is loud, and it needs skilled maintenance and a supply chain for the hot section. A diesel driving a screw compressor is heavier and larger for the same flow and slower to come up, but it is markedly cheaper to run, easier to maintain with ordinary skills, and far more tolerant of neglect and of poor fuel. For a busy main base launching formations, the turbine's flow and recovery usually win. For a smaller unit, a detachment, or an operator who values self-sufficiency over launch tempo, the diesel is often the better machine to actually own. And where the fleet is small aircraft or helicopters, the honest answer may be neither — a compact portable starting unit may cover the requirement at a fraction of the cost.
Q · 05 Why is the hose treated as a design problem?
Because it silently eats the performance you paid for, and because it is the part a person has to wrestle with. Three things happen in a large-bore duct. First, pressure drop: at these flows, a hose that is slightly too small or slightly too long can consume a meaningful share of the delivery pressure, so the cart's certificate says one thing and the aircraft receives another — which is why the rating should be quoted at the coupling. Second, volume: the hose's own internal volume has to be filled before full flow reaches the aircraft, which delays the start of useful cranking. Third, and least glamorous, handling: the duct is bulky, stiff in cold weather, hot after a start, and awkward to coil. If stowage was an afterthought, it ends up dragged across an apron, damaged at the coupling, and eventually leaking — at which point performance quietly degrades and nobody connects the two. So bore and length are chosen with the pressure drop calculated, the coupling is specified for repeated connection in gloves, and a cradle or reeler is designed in so that one person can deploy and stow it in wind and rain without help.
Q · 06 What do you build, and what is bought in?
Divided honestly. What Neometrix provides: the trolley structure and running gear — chassis, drawbar and tow eye, suspension, brakes, wheels and tie-down provisions; the complete air path — ducting, valves, filtration, water separation and silencing, laid out for minimum loss; hose management and the ground connector interface, including cradle or reeler and stowage; the controls and protection — start sequencing, overspeed, over-temperature and low-oil-pressure trips, automatic shutdown, clean abort, and an operator panel usable in gloves and rain; the weatherproof and acoustically treated enclosure; assembly and integration; performance testing — flow at delivery pressure, hot-day derate, consecutive-start duty and protection-trip proving; and commissioning, documentation, operator training, spares and AMC. What is bought-in certified: the prime mover, whether gas turbine or diesel, the compressor, filter elements, transducers, and wheel and braking components. What is not ours: the aircraft's own air turbine starter and its engine — we deliver air to the coupling to a specification, and the aircraft side belongs to the airframer. Engineered to order; quoted across jet air starter, portable engine-starting unit and starting-trolley requirements; no delivered starter trolley is claimed on this page.
Related

The ground support family from Neometrix.

The same apron, different services — engineered at our Noida facility.

Browse all Neometrix product lines.

Get a quotation

Send the start-air demand
and the airfield.

The projects desk replies within two working days with a clause-by-clause compliance matrix and a budgetary quotation. Write to [email protected] or use the form.

Enquire — jet air starter trolley Capability sheet (PDF) +91 7777 876 876
ISO 9001 / 14001 ENGINEERED TO ORDER — JET AIR STARTER TROLLEY FLOW HELD AT PRESSURE · RATED HOT AND HIGH · STARTS PER HOUR · QUOTED AT THE COUPLING ENGINEERED IN NOIDA · INDIA
JET AIR STARTER TROLLEY · TURBINE + DIESEL AIR START UNITS · PORTABLE ENGINE-STARTING UNITS · OVERHAUL, RE-POWER & AMC +91 7777 876 876 Enquire

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