Custom die-cut isolation & damping parts · for avionics, interiors & equipment integrators

Aircraft Vibration, NVH & Shock Isolation

Avionics equipment rack in an aircraft equipment bay where die-cut isolation pads and tray liners carry the mounted electronics

H-O Products die-cuts and converts PORON microcellular urethane, vinyl nitrile, neoprene and silicone foams, rebonded elastomer, pressed felt, and mass-barrier silicones into isolation pads, shock mounts, BSR details, and acoustic treatments for airframes, built to your drawing. Equipment-level vibration qualification (the MIL-STD-810 and DO-160 vocabulary) stays with the equipment maker; the materials and their TDS data are cited throughout.

Built for: avionics rack and LRU mounts, shelf and tray liners, interior panel and trim BSR control, equipment and gearbox-adjacent pads, acoustic damping and barrier stacks, and shock-attenuating details.

01
8 families
Isolation & damping families, one converter
PORON 4701 / 4790, ENSOLITE and SBE vinyl nitrile, SCE neoprene foam, HT-800 silicone foam, rebonded neoprene, SAE pressed felt, and A2 mass-barrier silicones.
02
5 bands
Disturbance bands on the ladder
Taxi and gust, propeller orders, rotor harmonics, gearbox and accessory orders, and broadband acoustics, each asking a different question of the mount.
03
5 zones
Isolation zones covered
Avionics racks and LRU mounts, interior panels and trim, equipment and engine-adjacent pads, acoustic treatments, and shock details.
04
11
Standards cited
MIL-STD-810 and RTCA DO-160 qualitatively, SAE AS8049 by designation, ASTM D3574, D1056, D2632, D395, C423, FAR 25.853 context, and the vendor TDS series, referenced inline.
Made in Winsted, CT · Family-owned since 1971 · ISO 9001:2015 certified organization
Finished die-cut PORON 4701 / 4790 Microcellular Urethane parts converted by H-O Products, on release liner ready to ship
How it works
  1. 1
    Send drawing
    Upload a DXF, STEP, or PDF, or describe the mount: what is mounted, what shakes it, and where it lives.
  2. 2
    Material review
    Engineering reviews the disturbance band, the mounted mass against the pad's load range per the TDS, compression set, the temperature and fluid environment, and any fire callout.
  3. 3
    Prototype
    Samples typically ship in 3–5 business days for common die-cut configurations on materials we keep on hand. Made-to-order; MOQ varies by material and part.
  4. 4
    Production
    Standard production runs ship about 2 weeks after drawing approval, including kiss-cut PSA-backed pads and kitted shipsets, with material traceability and lot-code TDS records.
Quick Answer

To isolate aircraft equipment, put the mounted natural frequency well below the disturbance band. For avionics racks and LRU mounts against rotor and propeller orders, specify soft cellular urethane: PORON 4701 / 4790 grades, sized so the mounted mass sits in the pad's working range per the TDS. For interior BSR details, use thin low-set pads: PORON or vinyl nitrile. For hot or oily locations, move to silicone foam, neoprene foam, or SAE felt.

For broadband acoustics, switch from isolation to damping and mass barriers (A2 barrier silicones). Values per the TDS on file; equipment-level qualification stays with the equipment maker.

Standards & Test Methods

MIL-STD-810 (environmental test methods incl. vibration and shock, qualitative) · RTCA DO-160 (airborne equipment vibration / shock categories, qualitative) · SAE AS8049 (seat performance standard, by designation for seat-adjacent cushioning) · ASTM D3574 (flexible cellular PU test methods) · ASTM D1056 (sponge grading and CFD) · ASTM D2632 (resilience by rebound) · ASTM D395 (compression set) · ASTM C423 (sound absorption) · FAR 25.853 (interior materials context) · the Rogers PORON and vendor foam TDS series behind the values.

When To Spec What
NVH · SHOCK / VIBRATIONDie-cut pad damps equipment vibrationvibrating equipmentdie-cut isolation padquiet mount
H-O isolation pads to the mount so equipment vibration is absorbed before the airframe.
Converted isolation & damping materials · Where it lives

Application Zones

Five vibration problems share one airframe and refuse one solution: the avionics mount that must isolate rotor orders, the trim joint that must stop squeaking, the gearbox-adjacent pad that must survive heat and oil while it works, the cabin wall that must lose decibels, and the shock event that must be absorbed once and recovered from.

Click a tab to see the job, the controlling properties, and the families H-O converts for that zone across the aerospace & defense programs we support; the deeper physics lives on our NVH & vibration control overview.

Avionics tray and mount detail with isolation pads between the equipment and the rack structure

Avionics rack, shelf & LRU mount isolation

Test methods: ASTM D3574 (PU), D1056 (sponge)Context: equipment qualified per DO-160 / MIL-STD-810 categories by the maker

The avionics mount's job is frequency separation: the loaded natural frequency of the pad-plus-box system has to sit well below the airframe's strong disturbance bands so the mount attenuates rather than amplifies. At LRU and shelf masses, soft microcellular urethane gets there in thin sections: the PORON 4701 ladder spans very soft through firm with low compression set per the TDS, and the V-0 grade carries the fire-class callouts equipment bays ask for.

Load matching is the discipline: each grade has a working stress range on its TDS, and a pad loaded too lightly is a stiff shim while one crushed past range is a dead one. The ladder tool above maps the band logic; the equipment's vibration qualification categories (DO-160 section 8, MIL-STD-810 methods) belong to the equipment maker and tell the converter which bands matter. [2] [4]

PORON 4701 SeriesThe shelf-pad ladder: 4701-30 very soft, 4701-40 V-0, 4701-50 firm; properties per ASTM D3574 on the TDS. [10]
PORON 4790-92 Slow ReboundExtra-soft, energy-absorbing grade (4790-92) for mounts that see both vibration and handling shock.
SBE Vinyl NitrileClosed-cell VN pads (SBE41VN, SBE42VN) with resilience data per ASTM D2632; the economical tray-liner ladder. [6]
SCE Neoprene FoamRugged closed-cell neoprene (SCE41BSCE43B) for mounts that also see oil mist and handling abuse.
Aircraft cabin interior panels during installation where thin pads silence buzz squeak and rattle at the joints

Interior panel, trim & monument BSR control

Problem: buzz, squeak, rattle at micro-motion jointsContext: interior materials carry FAR 25.853-type data per TDS

Cabin noise complaints are mostly not airframe physics; they are joints. Panel-to-panel contacts, bin latches, monument interfaces, and trim edges move fractions of a millimeter with every vibration cycle, and each dry contact is a potential squeak or rattle.

The cure is a thin, soft, low-compression-set interface pad that keeps the joint loaded and converts the micro-motion into silent shear: kiss-cut PSA-backed PORON and vinyl nitrile details are the standard answers, applied at the contact points the trim drawings mark. Interior placement brings the fire context: the FAR-referenced vinyl nitrile grades and the V-0 PORON entries keep the BSR fix inside the program's materials tent.

The converting format is the point here: hundreds of small pads per shipset, kiss-cut on liner, kitted by installation zone so the line pulls one part number per panel run. [9]

ENSOLITE Vinyl NitrileTrim and bin contact pads; MLC Black carries a FAR 25.853 Appendix F Part I (a)(1)(ii) pass per TDS (40% compression set, 200 °F), IG1 UL 94 HF-1 / V-0 only. Where a cabin-side pad carries the fire callout and must hold set, kSil KSV001KSV006 silicone sponge brings FAR 25 Appendix F, ABD0031, smoke and toxicity data and 1% compression set per TDS.
PORON 4701 Thin SectionsFine-celled urethane in thin gauges for tight trim gaps; very low set keeps joints loaded for years.
SAE Pressed FeltThe classic anti-squeak interface (F-1, F-26); compressible, high-friction, and quiet against hard trim.
Cork Wonder PadsSelf-adhesive cork-elastomer pads for point contacts and shipping-adjacent protection inside monuments.

Equipment, gearbox-adjacent & hot-zone pads

Drivers: temperature and fluids first, then frequencyTest methods: ASTM D1056; heat aging per TDS

The same isolation job moves to different materials when the location turns hostile. Near gearboxes, bleed runs, and engine accessories, urethane's comfort zone is exceeded: silicone foam (the HT-800 ladder) keeps its spring across a wide published window, neoprene foam takes oil mist and abuse economically, and pressed felt remains the quiet veteran for high-load, high-friction interfaces that must tolerate contamination.

Heavy equipment bases (pumps, blowers, support equipment racks) sit on thick rebonded-neoprene pads whose mass and internal friction eat structure-borne transmission. Where mist becomes wetting, the material logic hands off to the fluid-zone page; where the pad also carries a fire callout, the silicone families bring their TDS data with them. Frequency still matters; environment just votes first. [5]

BISCO HT-800 Series Silicone FoamThe hot-zone ladder (HT-870, HT-800, HT-820); UL 94 V-0 / HF-1 and flame-spread / smoke data per TDS. For cabin-side pads that need FAR 25 Appendix F, ABD0031, smoke and toxicity data with 1% compression set, the kSil KSV001KSV006 silicone sponge ladder is the documented pick.
SCE Neoprene FoamOil-tolerant, rugged isolation (SCE42B, SCE45B firm) per ASTM D1056 grading.
SAE Pressed Felt (F-grades)Dense wool felt (F-10) with a −62 to +93 °C class window per TDS; high-load pads and wicking-tolerant interfaces.
Rebonded NeopreneThick, high-mass base pads (25 class, 27 class) for equipment feet and support-structure interfaces.
Acoustic damping and barrier treatment applied to aircraft panel structure to cut broadband cabin noise

Acoustic damping, absorbers & mass barriers

Test method: ASTM C423 (absorption) per TDSTeaching: broadband noise is not an isolation problem

The band ladder's top rung is the honest one: broadband acoustic energy sits above any practical mount frequency, so the tools change.

Three mechanisms carry cabin and bay acoustics: damping, where a lossy layer bonded to a panel converts its flexural vibration to heat; absorption, where open or semi-open foams eat reflected energy (quantified per ASTM C423 on insulation TDS entries); and mass barriers, where a dense limp layer (the A2 barrier silicones) blocks transmission, with the fiberglass-reinforced A2 entry carrying FAR 25.853 / 25.856 references for cabin-side stacks.

Converted reality: these ship as laminations, barrier plus absorber plus facing cut as one part, coordinated with the FST materials page when the stack carries fire callouts and with the insulation pages when it joins the blanket system. [8]

BISCO A2 Sound BarrierDense limp-mass silicone (A2, A2 reinforced); FAR references on the reinforced TDS entry.
Silicone Foam Damping LayersConformable lossy layers for panel damping where temperature or fire data rules out organics.
Vinyl Nitrile Absorber FoamsClosed and semi-open VN grades for absorber layers in trim-side stacks; MLC Black is the grade with a FAR 25.853 reference per TDS.
Insulation-system stacksWhere the acoustic treatment joins the thermal blanket system, the cabin-insulation page carries the system logic.

Shock attenuation & transport protection

Problem: single events, not steady vibrationMaterials: energy-absorbing urethanes, slow-rebound grades

Shock is a different contract than vibration: one large event (hard landing, handling drop, transport impact, gunfire-adjacent transient on defense platforms) that the pad must absorb without bottoming and then recover from.

Energy-absorbing urethanes own this: the slow-rebound PORON grades (4790-92 class) and the ShockSeal family are engineered to spread the impulse over time and distance, and thin ShockPad-class films protect displays and PCBs inside equipment. The design discipline is travel: a shock pad needs enough thickness and the right firmness so the event uses most of the stroke without slamming the stops; the TDS impact data per grade is the screening evidence.

Equipment-level shock categories (DO-160 section 7, MIL-STD-810 shock methods) define the event; the seat-and-restraint world has its own standard vocabulary (the AS8049 context) that seat-adjacent cushioning is reviewed against. [1] [3]

PORON 4790-92 Slow ReboundThe energy-absorbing workhorse (4790-92); impact behavior per the TDS.
PORON ShockSeal 4790-79Sealing-plus-shock grade (ShockSeal 4790-79) for covers that must do both jobs in one part.
Rebonded Neoprene BlocksThick crush-tolerant pads for transport bases and ground-support protection.
High-shock defense electronicsWeapon-bay and high-shock avionics protection carries its own page in the defense set.
Isolation pad converting · Spec discipline

Six decisions that drive your isolation spec

Isolation selection is frequency physics wearing a materials catalog. The right pad puts the mounted natural frequency where the math wants it, at the real mass, in the real environment, for the life of the airframe, and the classic failures all come from optimizing firmness while ignoring one of those qualifiers. The deeper SDOF treatment lives on our NVH overview; the factors below are the aircraft-specific cut.

Specification principle

Isolate below the band or stop calling it isolation. A mount whose natural frequency sits inside the disturbance band amplifies; near it, it resonates; only well below does it isolate. Find the band first, and when the band is broadband acoustics, change tools instead of materials.

√2
The crossover: isolation only begins when disturbance frequency exceeds the natural frequency by this ratio

Below that ratio every mount transmits more than it blocks, and at resonance it multiplies the input. The qualitative consequence drives this whole page: softer pads and more deflection push the natural frequency down, and the ladder tool shows which bands you can realistically get below with a converted pad.

PORON 4790-92 Extra-Soft Slow Rebound MethodsASTM D3574 series per TDS Setvery low, per TDS Characterenergy-absorbing, slow rebound Formatsdie-cut, kiss-cut, PSA-backed

Read the six factors below in order. Band first, then load, then life, then environment; the damping-versus-isolation fork and the fire callout finish the spec. Every step has a TDS number behind it.

Show all 6 selection factors tap to expand
1

Find the disturbance band before picking any material

Propeller orders, rotor harmonics, gearbox meshes, taxi and gust inputs, and broadband acoustics each live in different parts of the spectrum, and the mount's one job is to put the loaded natural frequency well below the lowest band that matters.

The equipment's qualification categories (DO-160 vibration curves, MIL-STD-810 methods) and the platform's known orders name the band without any measurement campaign. Start every isolation conversation with "what frequency is the enemy"; the ladder tool exists because that one answer routes the whole selection. [2]

Qualification categories are equipment-level and belong to the equipment maker; they are cited here as the source of the band, not as a material claim.
2

Load-match the pad: the TDS stress range is the contract

A foam pad is a spring only inside its working stress range. Under-loaded, it barely deflects and the natural frequency stays high; over-loaded, it densifies and turns into a stiff shim with a memory problem. Every grade on this page publishes its range (CFD per ASTM D1056 for sponges, the D3574 suite for urethanes), and the pad area is your design variable: shrink the footprint to raise stress into range at light masses, spread it for heavy gear.

Send the real mounted mass with the drawing; "about a kilogram" picks a different grade than "about ten." [4]

Working ranges per the TDS on file; first-article deflection under real load is the cheap verification.
3

Compression set decides whether year five works like day one

An isolation pad spends its service life compressed, and permanent set is stiffness drift: as the pad flattens, deflection shrinks, natural frequency climbs, and the mount slowly walks back toward the disturbance band it was specified to avoid.

The low-set families (PORON urethanes, silicone foams) publish their numbers per ASTM D395 / D3574 precisely because this drift is the life-limiting mechanism. Compare set at the service temperature, not the lab number, and treat any grade without published set data as disqualified for permanent mounts. Felt and rebonded pads play by different rules (fiber consolidation), which their long history calibrates. [7]

Set values per the TDS on file; re-torqued mounts after set are a symptom, not a maintenance plan.
4

Temperature and fluids veto the default urethane

PORON owns the benign bays; the airframe has other neighborhoods.

Gearbox-adjacent and bleed-adjacent locations run past urethane's comfort window, where the HT-800 silicone foam ladder keeps its spring per its published class; oil-misted zones favor neoprene foam and felt; and genuinely fluid-wetted mounts leave this page for the fluid-zone selection logic. Write the measured local temperature and the fluid exposure on the drawing, and let them veto before frequency fine-tuning begins.

The same SDOF physics applies to every family; the environment just decides which family is still elastic in five years. [11]

Service windows per the TDS on file; the felt grades publish a −62 to +93 °C class, the silicones wider.
5

Know when the job is damping or mass, not isolation

Three different physics hide under "make it quieter." Isolation (this page's ladder) separates a mass from a vibrating base and works below the band. Damping bleeds energy out of a resonating panel and works at the panel's own modes: a bonded lossy layer, not a mount.

Mass barriers block airborne transmission and work by sheer limp weight: the A2 silicone barriers. Diagnose which mechanism your decibels need before buying anything: an isolation pad under a ringing panel does nothing, and a mass barrier on a shaking shelf just shakes heavier. The acoustic zone above carries the handoff. [8]

Absorption coefficients per ASTM C423 appear on insulation TDS entries; barrier mass per the A2 TDS.
6

Interior placement adds the fire-data requirement

An isolation or BSR pad inside the cabin or a cabin-adjacent bay inherits the interior-materials context: the program will ask what flammability data stands behind it.

The families on this page answer differently: PORON's V-0 grade, the FAR 25.853-referenced ENSOLITE MLC Black entry, the kSil KSV sponge's FAR 25 Appendix F / ABD0031 / smoke / toxicity entries, and the silicone foams' flame and smoke data all live on their TDS, while commodity foams answer with silence. Carry the fire callout into the pad spec from the start (the FST materials page maps the clause logic), because retrofitting paperwork onto a thousand installed BSR pads is nobody's favorite program. [9]

Decision support
Instrumentation·Interactive Selection

Specification Tools

Two stops to take you from "this thing shakes" to here's what to put on the drawing: a natural-frequency band ladder that locates your disturbance and shows where the mount has to sit, and a side-by-side comparison matrix of every family on this page.

1. Isolator natural-frequency band ladder (qualitative SDOF teaching)

Pick the dominant disturbance band. The ladder marks it, shades the region where the mounted natural frequency has to sit (well below the band, past the crossover), and returns the material direction that typically gets there at converted-pad masses. Ordinal bands only: no frequencies or transmissibility values are computed, and the mounted mass and pad geometry set the real number.

Why this toolMost isolation missteps are band errors, not material errors: a pad picked by feel sits inside or above the disturbance band and amplifies. The ladder makes "below the band" a visible, checkable location before any firmness argument starts.
Dominant disturbance
Higher frequencyThe ladder (ordinal bands)
Broadband acoustic energy
Gearbox / accessory orders
Rotor / engine harmonicsDisturbance band
Propeller-order bandTarget fn region
Taxi / runway / gust bandTarget fn region
Below all strong inputsTarget fn region
Lower frequencyMount natural frequency wants to live down here

Engine / rotor harmonics: the standard avionics isolation case

Turbine and rotor harmonic bands give the isolator room: a soft-to-medium pad whose loaded natural frequency sits in the bands below typically clears the crossover with margin. This is where most LRU shelf pads, tray liners, and equipment mounts live, and where the firmness ladders earn their keep, chosen against the real mounted mass per the TDS load range.

Dominant disturbanceWhere the mounted fn must sitMaterial direction
Taxi / runway / gustVery low; deep-deflection territoryExtra-soft slow-rebound urethane + structural review; sometimes damping is the honest answer
Propeller ordersComfortably below the 1P bandPORON 4701-30 class, soft vinyl nitrile, soft silicone foam
Rotor / engine harmonicsIn the bands below, with marginPORON 4701-40 V-0 / 4701-41 class (5–10% and 1.5–2.5% set per TDS) for permanently loaded mounts; SBE42VN (25% set, 160 °F) and SCE42B for tray liners and light duty
Gearbox / accessoryEasily below; environment votes firstHT-800 silicone foam, SCE neoprene, F-grade felt
Broadband acousticNo practical mount sits below itSwitch tools: A2 mass barriers, damping layers, absorbers
The ladder is ordinal and qualitative: it teaches the below-the-band rule (isolation begins past the crossover ratio) without computing frequencies, because the loaded natural frequency depends on the mounted mass, pad geometry, and the grade's stiffness per its TDS [4]. Equipment vibration categories (DO-160, MIL-STD-810 vocabularies) identify the bands and belong to the equipment maker [1]; pad sizing against your real mass is an engineering-review item with the TDS in hand.

2. Side-by-side: isolation & damping family comparison matrix

Every family called out on this page, with relative softness position, construction, the data position on its TDS, and the job it owns. Click a column header to sort. Click any material name to jump to its accordion entry and full TDS reference.

Filter
Material Softness (rel.) Construction Data position (per TDS) Owns
Isolation pads (frequency-separation duty)
PORON 4701 Series (30 / 40V0 / 50)Microcellular urethane ladder
5–7
Microcellular PU D3574 suite; UL 94 V-0 grade; low set LRU shelf & tray pads
SBE / ENSOLITE Vinyl NitrileEconomical closed-cell ladder
4–6
Closed-cell VN D1056, D2632 resilience; FAR ref on MLC Black Tray liners, trim pads
BISCO HT-800 Silicone FoamHot-zone isolation ladder
4–6
Cellular silicone D1056; E162 / E662 data; wide window Hot / fire-callout zones
SCE Neoprene Foam (41B/42B/43B/45B)Rugged, oil-tolerant
3–5
Closed-cell CR D1056; UL 94 HF-1 class entries Oily / rugged mounts
Interface, BSR & acoustic members
SAE Pressed Felt (F-1 / F-10 / F-26)High-friction quiet veteran
2
Pressed wool felt D2475 / D461 class data; −62 to +93 °C Anti-squeak, high load
Cork Wonder PadsSelf-adhesive point pads
1
Cork-elastomer Per TDS Point contacts
BISCO A2 Sound Barrier (+ reinforced)Limp-mass transmission block
n/a
Dense barrier silicone FAR 25.853 / 25.856 refs on reinforced Acoustic mass layers
Shock & base pads
PORON 4790-92 / ShockSeal 4790-79Energy-absorbing grades
7
Slow-rebound PU Impact / set data per TDS Shock events
Rebonded Neoprene (25 / 27 class)High-mass base pads
2
Rebonded elastomer Per TDS Equipment bases
Notes. Softness positions are relative orderings of the firmness ladders on each family's TDS, for sorting only; the A2 barrier is listed "n/a" because it is selected on mass, not softness. Data-position entries describe what the maker publishes (ASTM D3574 / D1056 / D2632 values, UL 94 classes, FAR-type references); equipment vibration and shock qualification belongs to the equipment maker. Verify every value against the TDS on file before final spec.
Found your candidate family? The fastest next step is the drawing: H-O reviews it against these selections and comes back with a manufacturable option and the TDS.
Already know your spec?

Skip ahead and request your engineering review now

If your drawing already calls out a PORON grade, a vinyl nitrile class, silicone foam, felt, or an A2 barrier stack, send it over for engineering review.

What goes wrong in the field

Isolation failures you can prevent at spec

Vibration fixes fail quietly and get blamed loudly. The pad ships, the equipment passes acceptance, and months later the fault log, the squeak report, or the cracked bracket tells the real story. Five patterns cover most of what goes wrong with converted isolation and damping parts, and all five are decided before the first part is cut.

Field caution

A wrong mount is worse than no mount. A pad whose natural frequency lands near the disturbance band amplifies the input it was bought to block. When vibration gets worse after an isolation fix, suspect resonance, not bad luck.

Show all 5 failure modes tap to expand

1. The mount resonated inside the disturbance band

A pad chosen by feel and firmness put the loaded natural frequency squarely in the platform's strong band, and the mount turned amplifier: the equipment saw more vibration than hard-mounting would have given it, connectors fretted, and the fix got blamed as "isolation doesn't work here." The fix: locate the band first (the equipment's DO-160 / MIL-STD-810 vibration categories and the platform's known orders name it), then select softness and deflection to put the mounted frequency well below it, past the crossover.

The ladder tool exists for exactly this check, and a first-article deflection measurement under real mass verifies the landing zone cheaply. [1]

2. The pad was load-mismatched and never worked as a spring

The same grade went under a half-kilogram sensor and a fifteen-kilogram box because it "worked last time." Under the sensor it barely deflected and isolated nothing; under the box it crushed into densification, took massive set, and turned into a shim.

Both installs failed with the same part number for opposite reasons. The fix: load-match per the TDS working range, using pad area as the design variable: small footprints raise stress into range for light gear, spread footprints carry heavy gear. Send the real mounted mass with the RFQ; the grade and the footprint come back matched, and the firmness ladders exist so the answer is a selection rather than a compromise. [4]

3. Compression set walked the mount back into resonance

A correctly specified mount drifted: years of compression took their permanent set, the working deflection shrank, the natural frequency climbed, and the system slid back toward the band it was designed to avoid.

The fault log shows a slow rise in vibration-related squawks with no event to blame. The fix: spec from the set data, not just the firmness: the low-set families (PORON, silicone foam) publish their numbers per ASTM D395 / D3574 at temperature, and the difference between two visually identical foams can be the whole service life. Where set is inevitable, design the deflection budget with margin so year-ten still sits below the band. [7]

4. The squeak fix used the right material in the wrong format

A BSR complaint got answered with the correct soft pad, hand-cut oversize, edges proud of the trim line, adhesive wrinkled at install. Six months later the pads had migrated, the edges showed, and the squeak was back with a cosmetic complaint as a bonus.

The material was never the problem; the converting was. The fix: treat BSR as a precision die-cutting job: exact footprints to the trim drawing, kiss-cut on liner so installers place parts once and correctly, PSA selected for the substrate pair, and zone-kitted sets so the line installs the right pad at the right station. Hundreds of small parts done right is a converter's job description. [9]

5. An isolation pad was bought for an acoustics problem

The cabin was loud, so soft pads went under everything that could be lifted, and the decibels did not move: the noise was airborne and panel-radiated, broadband acoustic energy that no mount frequency can sit below.

Money went to isolation; the problem wanted mass and damping. The fix: diagnose the mechanism before the material: structure-borne narrowband inputs take isolation, ringing panels take bonded damping layers, and airborne transmission takes limp-mass barriers (the A2 silicones) and absorbers, quantified per ASTM C423 on the relevant TDS entries. The ladder's top rung hands off deliberately, and the acoustic zone on this page picks up the job. [8]

Reference

Material reference

Detailed positions for eight isolation and damping families referenced on this page: the PORON 4701 / 4790 urethanes that own shelf pads and shock details, the vinyl nitrile ladders for trays and trim, HT-800 silicone foam for hot and fire-callout zones, SCE neoprene foam for rugged duty, SAE pressed felt for high-friction quiet interfaces, rebonded neoprene for bases, and the A2 mass barriers for acoustics. Methods are cited per family; numeric values are per the TDS on file, and H-O die-cuts, kiss-cuts, and kits every family to drawing.

PORON 4701 / 4790 Microcellular Urethane (30 / 40 V-0 / 50 / 4790-92 / ShockSeal)Isolation & shock anchor family · very low set · ASTM D3574 suite per TDS
CompositionMicrocellular polyurethane; standard (4701) and slow-rebound (4790) chemistries
Test methodsASTM D3574 series on the TDS; D2632-class resilience entries on energy grades
Compression setVery low across the rated window, per TDS; the family's defining property
Fire classUL 94 V-0 on the 4701-40 V-0 grade per TDS
Grades4701-30 · 4701-40 V-0 · 4701-41 (1.5–2.5% set @ 70 °C per TDS) · 4701-50 · 4790-92 · ShockSeal 4790-79
Form factorsDie-cut pads, kiss-cut PSA-backed sets, thin-section liners, zone kits
Where it lives in this application: LRU shelf and tray pads, equipment mount interfaces, BSR details in thin sections, and the shock-absorbing details (4790-92, ShockSeal) where a single event must be eaten and recovered from. The working-stress ranges on the TDS make load-matching a lookup instead of a guess.

PORON is the page's anchor because its defining property is the one this application lives on: compression set low enough that year-ten deflection still resembles day-one. The D3574 data per grade is the sizing evidence; match the mounted mass to the working range and let footprint do the tuning.

Vinyl Nitrile Foam (SBE41VN / SBE42VN + ENSOLITE IG / MLC)Economical closed-cell ladder · D2632 resilience data · FAR 25.853 App. F pass on MLC Black
CompositionClosed-cell vinyl nitrile (PVC / NBR blend) foams
Test methodsASTM D1056 grading; resilience per ASTM D2632 on SBE entries
Fire dataUL 94 HF-1 / V-0 classes on the IG grades; FAR 25.853 Appendix F Part I (a)(1)(ii) pass on the ENSOLITE MLC Black TDS (40% compression set)
CharacterDamped, economical, broadly tolerant; the value ladder of the page
Form factorsDie-cut tray liners, trim pads, kiss-cut BSR sets
Where it lives in this application: tray and shelf liners at moderate masses, interior trim and bin BSR pads (where the FAR-referenced MLC Black grade keeps the paperwork clean), and the wide middle of the isolation catalog where urethane performance is not required and urethane price is not welcome.

Vinyl nitrile is the page's value family: inherently damped, closed-cell, graded per D1056 with resilience numbers per D2632, and carrying a FAR-referenced entry (MLC Black) where interior placement demands it. It gives up set performance to PORON (SBE42VN 25% set, −20 to 160 °F per TDS); for permanently compressed precision mounts, read factor three before choosing it.

BISCO HT-800 Series Silicone Foam (HT-870 / HT-800 / HT-820 / HT-840)Hot-zone & fire-callout isolation · flame / smoke data per TDS
CompositionClosed-cell cellular silicone, four-firmness ladder
GradingASTM D1056; tensile per D412 on the TDS
Fire dataUL 94 classes with ASTM E162 / E662 flame and smoke entries per TDS
TemperatureWide silicone service window per TDS; the reason it owns hot zones
GradesHT-870 · HT-800 · HT-820 · HT-840
Form factorsDie-cut pads and washers, laminated to barriers and foils
Where it lives in this application: gearbox- and bleed-adjacent mounts, cabin-side pads carrying fire callouts, and every isolation position whose temperature or flammability requirement disqualifies the urethanes. The four-grade ladder keeps load-matching available at temperature.

HT-800 silicone foam is the same isolation physics in a chemistry that shrugs at heat and brings flame and smoke data to interior reviews. It costs more than urethane and earns it only where the environment says so; the zones above mark exactly where that is.

SCE Neoprene Foam (41B / 42B / 43B / 45B)Rugged, oil-tolerant isolation · ASTM D1056 graded · HF-1 class entries
CompositionClosed-cell neoprene (polychloroprene) blend foam ladder
GradingASTM D1056; resilience per D2632 on the TDS
Fire classUL 94 HF-1 entries per TDS
CharacterTough, abuse- and oil-mist-tolerant; the rugged middle of the catalog
GradesSCE41B · SCE42B · SCE43B · SCE45B
Form factorsDie-cut mount pads, washers, strip
Where it lives in this application: equipment mounts in bays that see oil mist, handling abuse, and ground-crew reality; gear-adjacent pads below silicone temperatures; and anywhere a tray liner needs to survive being stood on.

SCE neoprene is the page's work boot: not the softest, not the lightest, but graded, fire-classed, and hard to kill. Truly fluid-wetted mounts still leave for the fluid-zone page; mist and abuse stay here. Values per the TDS on file.

SAE Pressed Felt (F-1 / F-10 / F-26 Grades)High-friction quiet interfaces · −62 to +93 °C class · D2475 / D461 data
CompositionPressed wool felt, SAE density grades
Test methodsASTM D2475 / D461-class felt methods per TDS
Temperature−62 to +93 °C class window on graded entries per TDS
CharacterDense, high-friction, contamination-tolerant, naturally damped
GradesF-1 · F-10 · F-26
Form factorsDie-cut pads, washers, strips, wicking and wiping details
Where it lives in this application: high-load anti-squeak interfaces, control-run and linkage rub points, and pads that must keep working through oil, dust, and decades. The oldest material on the page and still unbeaten at its specialty.

Felt damps by fiber friction rather than cell mechanics, tolerates contamination that ruins foams, and carries SAE density grading with a published temperature class. It is not a precision spring; it is the quiet, durable interface the rest of the catalog cannot imitate.

Rebonded Neoprene (25 / 27 Density Classes)High-mass base & transport pads · thick sections
CompositionRebonded neoprene granulate, high-density pad stock
CharacterHeavy, internally damped, crush-tolerant in thick sections
DataDensity-class properties per TDS
Form factorsWaterjet- and thick pads, machine and equipment bases
BoundarySupport equipment and bases, not precision avionics mounts
Where it lives in this application: equipment bases, ground-support and transport protection, and structure-borne breaks under heavy gear, where mass and internal friction matter more than a tuned natural frequency.

Rebonded neoprene is the blunt instrument done properly: thick, heavy, damped, and cheap per kilogram of vibration eaten. Precision mounts stay with the graded foams; bases and transport belong here. Values per the TDS on file.

BISCO A2 Sound Barrier (+ Fiberglass-Reinforced)Limp-mass acoustic layer · FAR 25.853 / 25.856 refs on reinforced entry
CompositionHigh-density barrier silicone; plain and fiberglass-reinforced
MechanismLimp mass blocks airborne transmission; pairs with absorbers and damping layers
Fire referencesFAR 25.853 / 25.856 references on the reinforced TDS entry
Form factorsDie-cut mass layers, laminated barrier-absorber stacks
Adjacent pageStack-level FST logic on the FST materials page
Where it lives in this application: the mass member of cabin and bay acoustic stacks, monument and sidewall noise treatments, and equipment-bay barriers, laminated with absorber foams and facings into single converted parts.

The A2 barriers carry the acoustic job that isolation cannot touch, inside the fire-documented materials tent. Acoustic performance is a stack property; H-O converts the stack as one part so the lab result and the installed part match.

Wonder Pads + Cork (Pre-Cut Separation & Isolation)Separation layers and anti-slip · D1056/D3575 classes · F36 cork compressibility
CompositionPre-cut cork and foam separation pads; natural and rubberized cork sheet
Grades hereWonder Pads in cork and 2# / 4# foam; cork MS113 plain and rubberized
MethodsThe 4# foam Wonder Pad reports its class per ASTM D1056/D3575; cork compressibility per ASTM F36
Form factorsPre-cut pads, separation layers, slit strips

Separation pads are appearance-critical as much as functional: a Wonder Pad keeps two finished faces from marking each other in transit.

Engineering questions

Aircraft isolation: engineer-grade FAQ

Twelve of the questions we hear most from equipment, interiors, and sustainment engineering teams. If your question isn't here, send a drawing or call, engineering picks up.

12 questions · click a question to expand its answer

How do I pick an isolation pad for an avionics box or LRU?

Three steps, in order. First, locate the disturbance band: the platform's propeller or rotor orders and the equipment's vibration categories name it. Second, choose the softness and thickness that put the loaded natural frequency well below that band; the ladder tool on this page walks the logic qualitatively.

Third, load-match: every grade has a working stress range on its TDS (ASTM D3574 for the PORON ladder), and pad area is the tuning variable, small footprints for light boxes, spread footprints for heavy ones. Send the mounted mass with the drawing and the grade-plus-footprint answer comes back matched. [4]

Why did vibration get worse after we added isolation pads?

Resonance. A mount only isolates above the crossover ratio; below it, it transmits, and at its own natural frequency it amplifies, sometimes dramatically. A pad chosen by feel commonly lands its natural frequency inside the platform's strong band and turns the mount into a multiplier, which is why a wrong mount is worse than no mount.

The fix is the ladder discipline: name the band, then drive the mounted frequency well below it with softness, thickness, and footprint, and verify the loaded deflection on a first article. If the input is broadband acoustic, no mount frequency works and the job changes to damping and mass barriers.

What is the difference between isolation, damping, and a mass barrier?

Three mechanisms for three problems. Isolation separates a mass from a vibrating base with a soft spring and works when the disturbance frequency is well above the mounted natural frequency: the pad-under-the-box physics. Damping bleeds energy out of a structure that is resonating: a lossy layer bonded to a ringing panel, effective at the panel's own modes. Mass barriers block airborne sound transmission with limp weight: the A2 silicone sheets in a sidewall stack.

Diagnose which one your problem is before buying material, because each mechanism's material does nothing for the other two jobs. [8]

What does MIL-STD-810 or DO-160 vibration testing mean for pad selection?

They are equipment-level test vocabularies, not material ratings: MIL-STD-810 methods and DO-160 section categories define the vibration and shock environments the equipment maker qualifies the box against. For the converter they are the most useful documents in the conversation, because the test curves name the frequency bands and levels the mount must beat. No pad is "MIL-STD-810 rated"; a mounted system passes its category with the pad's help.

Bring the category or curve to the drawing review and the band-ladder conversation becomes specific instead of qualitative. [1]

How do I silence buzz, squeak, and rattle in cabin trim?

Find the dry contacts and keep them loaded. BSR noise comes from micro-motion at panel joints, bin interfaces, and trim edges; the cure is a thin, soft, low-set pad at each contact that converts the motion to silent shear. The converting format is most of the battle: exact footprints to the trim drawing, kiss-cut on liner for one-step installation, PSA matched to the substrate pair, and zone-kitted sets so each panel run pulls one part number.

Interior placement adds the fire context: the FAR-referenced ENSOLITE MLC Black grade, kSil KSV silicone sponge and V-0 PORON entries keep the fix documented. [9]

Which pad materials survive next to a gearbox or in a hot bay?

Move up the temperature ladder: silicone foam first. The HT-800 series keeps its spring across a wide published window and brings flame and smoke data per its TDS; SCE neoprene covers the oil-misted, abuse-heavy middle below silicone temperatures; and SAE pressed felt remains the contamination-tolerant veteran with a published −62 to +93 °C class. Urethane stays in the benign bays where its set performance shines.

If the location is genuinely fluid-wetted rather than misted, the selection leaves this page for the fluid-zone logic. Measured local temperature beats bay averages on every drawing. [11]

What materials absorb shock events rather than steady vibration?

The energy-absorbing urethanes: slow-rebound PORON (4790-92 class) and the ShockSeal grades. Shock is a single large impulse, and the pad's job is to spread it over time and stroke without bottoming, then recover; slow-rebound chemistry does exactly that, with impact data per grade on the TDS. The design discipline is travel: enough thickness and the right firmness that the event uses most of the stroke.

Thin ShockPad-class films protect displays and boards inside equipment, and thick rebonded pads take transport and base duty. Equipment shock categories (DO-160 section 7, MIL-STD-810 methods) define the event the design must eat. [10]

Why did my isolation pad flatten, and what does compression set do to the mount?

Set is stiffness drift with a schedule. A permanently compressed foam slowly keeps some of that compression; as the pad flattens, its working deflection shrinks, the mounted natural frequency climbs, and the mount migrates back toward the disturbance band, which reads as a gradual rise in vibration squawks years after a clean install.

The drivers are material class (low-set urethanes and silicones versus commodity foams), over-compression past the working range, and temperature above the rated window. Spec from the published set data per ASTM D395 / D3574 at the service temperature, and budget deflection margin so year ten still sits below the band. [7]

Does seat cushioning fall under this page, and what is AS8049?

Adjacent, with a hard boundary. SAE AS8049 is the performance standard vocabulary for aircraft seats, and seat systems (including their energy-absorbing cushion builds) are certified by the seat maker under it; H-O does not supply certified seat systems or claim any part of that approval.

What we convert, as a materials supplier, are the cushioning, BSR, and comfort-adjacent foam details around interiors and monuments, reviewed against the program's flow-downs, with FAR-referenced grades where interior placement requires documentation. If your part is inside a certified seat build, your seat maker leads and we support their material spec. [3]

Do isolation pads need fire-rating data on aircraft?

Inside the cabin and cabin-adjacent bays, expect the question and carry the answer. Interior-materials context (the FAR 25.853 vocabulary) reaches pads, liners, and BSR details, and the program will ask what data stands behind each one. The families on this page answer on their TDS: the PORON V-0 grade, the FAR-referenced ENSOLITE MLC Black entry, the kSil KSV sponge (FAR 25 Appendix F, ABD0031, smoke and toxicity data), and the silicone foams' flame and smoke data.

Which clause applies to which part is the program's call, and the FST materials page maps that logic; the converter's job is supplying grades whose paperwork is ready when the question lands. [9]

Can H-O kit a full shipset of isolation and BSR parts?

Yes, and this application is where kitting pays fastest, because the parts are numerous, small, and station-specific. H-O and kiss-cuts the pad set, bags it by installation zone or work card, labels to your numbering, and ships one part number per kit with lot-coded TDS records per component, through our assembly & kitting capability. Interiors lines stop losing minutes to pad-hunting, MRO refresh kits match the shop visit instead of the warehouse, and material substitution stops happening at the bench because the right grade is the one in the bag.

What lead time should I expect for isolation-pad samples and production?

H-O is a die-cutter and converter, so every pad, liner, and barrier stack is made-to-order to your drawing, including samples. We maintain working material relationships with the urethane, vinyl nitrile, silicone, and felt makers and keep common stocks on hand for faster turnaround.

Samples typically ship in 3–5 business days for common configurations on materials we keep on hand. Standard production runs ship about 2 weeks after drawing approval, including kiss-cut PSA-backed sets and zone kits. Expedited service is available when line or retrofit dates are hard. MOQ varies by material and part; prototype quantities through production runs are equally accepted. Send the drawing and quantity through the form below for a specific commitment with your quote.

Last updated · Reviewed by H-O Products engineering (ISO 9001:2015 certified converter, Winsted, CT).

Citations

Standards, test methods & technical references

The standards, test methods, and vendor technical data sheets cited throughout this page. Standards editions current as of June 2026; verify against the publishing body before final spec. H-O converts materials tested to these methods on the source manufacturer's TDS; H-O does not independently certify materials, and equipment-level vibration and shock qualification remains with the equipment maker.

MIL-STD-810

Environmental Engineering Considerations and Laboratory Tests: the defense test-method standard whose vibration and shock methods define the environments equipment is qualified against. Cited qualitatively as the source of disturbance-band and event definitions, never as a material rating. quicksearch.dla.mil (MIL-STD-810)

RTCA DO-160

Environmental Conditions and Test Procedures for Airborne Equipment, including the vibration and shock sections whose categories name the bands and events airborne equipment must survive. Equipment-level by construction; cited qualitatively. rtca.org (DO-160)

SAE AS8049

Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft. Cited by designation to mark the boundary: seat systems and their energy-absorbing builds are certified by seat makers under this vocabulary; H-O supplies adjacent converted cushioning materials only. sae.org (AS8049)

ASTM D3574

Standard Test Methods for Flexible Cellular Materials, Slab, Bonded, and Molded Urethane Foams. The method suite behind the PORON property tables: CFD-type stiffness, compression set, and the working-range data load matching depends on. astm.org/d3574

ASTM D1056

Standard Specification for Flexible Cellular Materials, Sponge or Expanded Rubber. The grading and CFD framework behind the vinyl nitrile, neoprene, and silicone sponge ladders on this page. astm.org/d1056

ASTM D2632

Standard Test Method for Rubber Property: Resilience by Vertical Rebound. The bounce-versus-absorb number on the foam TDS entries: high resilience suits springs, deliberately low resilience marks the energy-absorbing shock grades. astm.org/d2632

ASTM D395

Standard Test Methods for Rubber Property: Compression Set. The permanent-deformation method behind the stiffness-drift discussion; read set at the service temperature on the TDS. astm.org/d0395

ASTM C423

Standard Test Method for Sound Absorption and Sound Absorption Coefficients by the Reverberation Room Method. The absorption vocabulary behind the acoustic-zone discussion and the insulation TDS entries it references. astm.org/c0423

FAR 25.853 (context)

Compartment interiors flammability requirements, cited as the context that reaches interior pads and BSR details. The clause-by-clause material map lives on the FST materials page; applicability is the program's determination. ecfr.gov (14 CFR part 25)

Rogers PORON 4701 / 4790 TDS

Rogers Corporation technical data for the PORON 4701 series, 4790-92 slow-rebound, and ShockSeal grades: D3574-suite properties, compression set, impact data, and the V-0 grade classification cited on this page. rogerscorp.com (PORON)

Vendor foam & felt TDS series (ENSOLITE / SBE / SCE / HT-800 / felt / A2)

The material makers' technical data sheets behind the remaining families: ENSOLITE and SBE vinyl nitrile (D1056 / D2632 data, FAR 25.853 reference on MLC Black), SCE neoprene foam, BISCO HT-800 silicone foam and A2 barriers, SAE felt grades (D2475 / D461-class data, temperature window), and rebonded neoprene. Values quoted qualitatively; TDS on file per lot. rogerscorp.com (BISCO)

Updated . Standards editions and links current at publication; verify against the publishing body before final spec. H-O converts materials tested to the methods cited; lot-specific material documentation available on request.

Quote request

Get a vibration & isolation materials quote

Send a drawing and the mounted mass. We typically respond within one business day with a material recommendation, prototype lead time, and TDS verification against your disturbance band, load, temperature, and fire callout.

Contact
Company address
Your application
Part & quantity
Typical response in one business day. Samples typically 3–5 business days; production in about 2 weeks.

Prefer to talk it through first? Contact the engineering team or call (860) 469-1144.

Continue reading

See also: related H-O aerospace pages

Engineering content for the adjacent aerospace materials problems. Each page covers material selection, failure modes, and converter-side process detail for its application family; the aerospace & defense hub maps the whole set.

Material data & standards. All firmness ladders, set values, resilience numbers, service windows, and flammability entries on this page are taken from the source manufacturers' technical data sheets and the cited standards; this page frames them qualitatively. The band ladder is an ordinal teaching aid: it computes no frequencies, and the loaded natural frequency of any real mount depends on mass, geometry, and grade stiffness per the TDS.

References to MIL-STD-810, RTCA DO-160, and SAE AS8049 are qualitative context for equipment- and seat-level qualifications that belong to their respective design holders; H-O makes no qualification claims. Verify against the vendor TDS and your own testing for your installation.

Conversion scope. H-O and converts foam, felt, and barrier stock to drawing in Winsted, Connecticut: die-cut and kiss-cut PSA-backed pads, thin-section liners, laminated barrier-absorber stacks, and zone-kitted shipsets, with material traceability and lot-code TDS records. H-O does not manufacture machined isolators, wire-rope mounts, or certified seat systems; those belong to their makers. Lead-time and MOQ details are on the process strip and in the quote form above.

Get Quote →