Component Derating Calculator
Component Derating Calculator
Derating is running a part below its rating so that it survives. The factors live in documents this page will not reproduce, so you type in your own — and what you get back is the arithmetic a single-factor calculation misses: the manufacturer’s own temperature curve has already taken part of the rating away before your factor is applied, and the two compound.
Applied stress against the derated limit, with the curve applied
a 0.25 W chip resistor whose curve is flat to 70 °C and runs to zero at 155 °C, sitting in an 85 °C box, dissipating 80 mW, with a 60% derating factor typed in from the reader’s own document
Two factors, and they multiply
allowance(T) = rating × frac(T)
derated(T) = rating × frac(T) × D
and a single-factor calculation returns rating × D, which is larger by 1 ÷ frac(T)
- D
- your programme’s derating factor, from your own copy of your own standard. This page will not supply it
- frac(T)
- the straight line on the data sheet: full rating to a knee temperature, then falling to an end value. For a resistor’s power that end value is zero; for a tantalum’s voltage it is a fraction of the rating
- R_th
- (Tend − Tknee) ÷ rating when it is derived from the curve, because at full rating in the knee ambient the hot spot is by definition at the end temperature
Worked example
a 0.25 W chip resistor whose curve is flat to 70 °C and runs to zero at 155 °C, sitting in an 85 °C box, dissipating 80 mW, with a 60% derating factor typed in from the reader's own document
At 85 °C the curve has already fallen to (155 − 85) ÷ (155 − 70) = 82.4% of the rating, so the manufacturer's own allowance there is 205.9 mW rather than 250 mW
The 60% factor applies to that, not to the nameplate: 205.9 mW × 0.60 = 123.5 mW
A single multiplication would have given 250 mW × 0.60 = 150 mW — 1.214× larger than the allowance that actually exists, and the whole of that gap is the temperature the reader is running at
So 80 mW is 64.8% of the real limit, where the single-factor answer would have said 53.3%. Headroom is 1.54×, and the ambient at which this dissipation uses the whole derated allowance is 109.7 °C
Separately, the curve implies a thermal resistance of (155 − 70) ÷ 0.25 = 340 K/W, so 80 mW lifts the film 27.2 °C above its surroundings to 112.2 °C, which is 12.8 °C below the 125 °C limit entered. A part can be inside its derated power and still too hot, and the two are separate findings
Where the factor comes from, and where it does not
| Document | Status | What it gives | How this page treats it |
|---|---|---|---|
| ECSS-Q-ST-30-11C Rev.2, 23 June 2021 | European Cooperation for Space Standardization; downloadable free, copyrighted | clause 5 sets out the principles and clause 6 holds the load ratios, one table per family — 6-1 to 6-9 capacitors, 6-13 to 6-15 diodes, 6-18 inductors and transformers, 6-24 relays and switches, 6-25 to 6-31 resistors, 6-35 to 6-38 transistors | cited by clause and table number; no value reproduced |
| NASA EEE-INST-002 | NASA Goddard instruction, controlled | part selection, screening, qualification and derating for three quality levels | cited; no value reproduced |
| MIL-STD-1547 | US military standard for space and launch vehicles | parts, materials and processes, with derating requirements | cited; no value reproduced |
| NASA GSFC PD-ED-1201, Preferred Reliability Practices | US Government work, may be reproduced | a single generic Table 1 — 60% of rated voltage for capacitors, 60% of rated power for resistors, 50% of rated power and 75% of rated voltage for semiconductors with a 110 °C junction cap, 80% of supply voltage and 75% of rated power for microcircuits with a 100 °C junction cap, 50% of rated voltage for inductive devices, 50% of rated current for relays and connectors | quoted, because it may be — and it is the source of this page’s default. It is a generic starting point, not your programme’s requirement |
| The part’s own data sheet | the manufacturer’s | the temperature curve: the knee, the end temperature and what is left there | taken as three reader inputs, because no two families share a curve |
Two factors that multiply, and the one that gets forgotten
Derating is the discipline of running a part below its rating so that it survives — longer, and through excursions the nominal design never sees. It is the single cheapest reliability measure there is, and on a spacecraft or a high-reliability programme it is not optional: the derating requirement is a contractual one, verified part by part in a review.
Why this page has no table in it. The factors live in ECSS-Q-ST-30-11C, in NASA EEE-INST-002 and in MIL-STD-1547, and those documents are copyrighted or controlled. They are also not interchangeable: they differ by part family, by quality level, by whether the application is benign or severe, and by programme. Reproducing a plausible-looking table here would give a reader a number that is wrong for their project and looks authoritative, which is worse than giving them nothing. So the page cites the clauses — ECSS-Q-ST-30-11C Rev.2 puts its principles in clause 5 and its load ratios in clause 6, one table per family — and asks you to type in the figure from your own copy. The one number it offers as a default comes from NASA Goddard’s Preferred Reliability Practice PD-ED-1201, which is a US Government work and may be quoted; its Table 1 is reproduced in full above, and it is a generic starting point rather than anybody’s requirement.
The arithmetic those documents leave to you. A derating requirement is a fraction of a rating, and a rating is a number stated at a condition. Almost every power, current and voltage rating is stated at a reference temperature, and the data sheet then draws a straight line: full rating up to a knee, falling to an end value at the maximum temperature. For a thick-film resistor that line runs from 70 °C to zero power at 155 °C, the maximum film temperature. For a solid tantalum’s voltage it runs from 85 °C to a fraction of the rating at 125 °C. Your factor applies to what the curve leaves, not to the nameplate, and the two compound. A 0.25 W resistor derated to 60% is not allowed 0.15 W in an 85 °C box; the curve has already taken it to 0.206 W, and 60% of that is 0.124 W. The single multiplication overstates the allowance by 1 ÷ frac(T), which at 85 °C on a 70/155 curve is 1.214 times. Run hotter and the gap widens fast.
The curve also tells you the thermal resistance, for free. At the full rating in the knee-temperature ambient the hot spot must by definition be at the end temperature, so R_th = (T_end − T_knee) ÷ rating. That is 340 K/W for a 0.25 W part and 42.5 K/W for a 2 W one — small parts are not merely weaker, they are thermally much worse. It is the number to reach for when a data sheet gives no thermal figure, and the page uses it unless you type a better one in. For a resistor specifically, the resistor power rating calculator does the same curve with the electrical side worked out for you; this page is the general case and the one to use when the stress is a voltage or a current rather than a power, or when the part is not a resistor.
What derating does not do. It does not turn a wear-out mechanism into a stress ratio. An aluminium electrolytic dies because its electrolyte dries out at a rate set by temperature, and no voltage derating changes that — see the ripple current and ESR calculator. A Class II ceramic loses most of its capacitance under DC bias, and derating the voltage changes where on that curve you sit rather than removing it — see the MLCC DC bias calculator. A solid tantalum’s voltage derating is about surge and ignition rather than about lifetime, and the circuit impedance decides how much is enough — see the tantalum derating calculator. Derating is necessary and it is not sufficient, and the failure modes it does not touch are the ones that catch people.
Frequently asked questions
Why does this calculator not just tell me the derating factor?
Because the factors are in ECSS-Q-ST-30-11C, NASA EEE-INST-002 and MIL-STD-1547, which are copyrighted or controlled and are not interchangeable. They differ by part family, by quality level and by programme, and a plausible-looking invented table would be worse than none. The page cites the clauses and does the arithmetic those documents leave to you. The one default it offers comes from NASA GSFC’s PD-ED-1201, which is a US Government work, and it is a generic figure to replace rather than to rely on.
Do I apply my derating factor before or after the temperature curve?
After — the factor applies to what the manufacturer’s curve leaves at your temperature. The two compound, and the page shows what the single multiplication overstates the allowance by. Some programmes instead take the smaller of the two limits rather than the product; the page reports that reading as well, so you can see which your document means.
My rating is quoted at 25 °C and my part runs at 85 °C. What do I use?
Set the knee to the temperature the rating is quoted at, the end temperature and end value to whatever the data sheet’s curve shows, and the reference temperature to the temperature at the part. The page then gives the allowance that actually exists there. A rating taken off the front page of a data sheet and used at 85 °C without the curve is the commonest single mistake in this whole subject.
What temperature should I type in — the ambient or the case?
Whatever the curve is drawn against, which the data sheet states, and measured where the curve says. For most small parts it is the ambient immediately around the part with everything else in the box running, not the room. In vacuum there is no ambient air at all: the reference is whatever the part conducts into, which is what the conduction-cooled electronics page is for.
Does derating a part make it last longer, or just make it safer?
Both, and they are different arguments. The safety argument is margin against an excursion the design did not anticipate. The lifetime argument is that most failure rates fall steeply with stress ratio — which is what PD-ED-1201’s Figure 1 shows. But derating does not touch a wear-out mechanism that is driven by something else: an electrolytic’s drying, a ceramic’s ageing, a solder joint’s thermal cycling.
Can I derate one stress and ignore the others?
No, and this is where parts get through review and fail in the field. A MOSFET has a drain-source voltage, a drain current, a dissipation and a junction temperature, and each is derated separately; the binding one is whichever comes out worst and it is often not the one the schematic draws attention to. Run the page once per stress.
Related calculators
References
- NASA Goddard Space Flight Center. Preferred Reliability Practices: EEE Parts Derating, Practice No. PD-ED-1201. A US Government work, freely distributed and reproducible. Table 1 gives generic derating guidelines — 60% of rated voltage for capacitors, 60% of rated power for resistors, 50% of rated power and 75% of rated voltage for semiconductor devices with a 110 °C junction cap, 80% of rated supply voltage and 75% of rated power for microcircuits with a 100 °C junction cap, 50% of rated voltage for inductive devices, 50% of rated current for relays and connectors — and Figure 1 shows piece-part failure rate against temperature for stress ratios from 1.0 down to 0.6. Verified against two independently hosted copies of the practice, which agree line for line. This is the source of this page’s default factor and junction-temperature limit.
- ECSS-Q-ST-30-11C Rev.2, 23 June 2021, Space product assurance — Derating — EEE components. Clause 5 sets out the principles of derating (5.2), applicability and component selection (5.3), the derating parameters and the requirements for transient and surge conditions (5.4). Clause 6 holds the tables of load ratios, one per family: 6-1 to 6-9 capacitors, 6-10 to 6-11 connectors, 6-13 to 6-15 diodes, 6-18 inductors and transformers, 6-24 relays and switches, 6-25 to 6-31 resistors, 6-35 to 6-38 transistors, 6-41 and 6-42 harness bundle derating. Clause structure verified against the published document; the values are copyrighted and are not reproduced here.
- NASA. EEE-INST-002: Instructions for EEE Parts Selection, Screening, Qualification, and Derating. The NASA derating instruction referenced by many US civil space programmes, with derating requirements by part family and quality level. Cited; not reproduced.
- MIL-STD-1547, Electronic Parts, Materials, and Processes for Space and Launch Vehicles. The US military standard whose derating requirements sit alongside the above on defence space programmes. Cited; not reproduced.
- Vishay. Solid Tantalum Capacitors (With MnO₂ Electrolyte) Voltage Derating, document 40246, revision 07 September 2022. The source of the shape of a voltage derating curve used as this page’s non-zero end-value example: the maximum working voltage equals the rated voltage from −55 °C to +85 °C and then falls linearly to two thirds of it at the 125 °C maximum working temperature.
- JEDEC. JESD51-12: Guidelines for Reporting and Using Electronic Package Thermal Information. The reason a thermal resistance has to be qualified by what it was measured against; the junction-to-ambient figure on a data sheet’s front page belongs to a standard test board. Cited by number; copyrighted and not reproduced.
