Contract Laboratory has received the following Aerospace Laboratory Test Requests which need to be fulfilled! These Laboratory Test Requests are received from a variety of sources ranging from start-up companies to large, multinational Fortune 500 corporations, international organizations, well-respected universities and government agencies that are actively seeking Independent, Third-Party Aerospace Laboratories to perform their Aerospace Testing, Analysis, Assays, Product Development, Scientific Research Experiments, Inspections, Certifications, and Engineering Projects. If you are a Aerospace laboratory that would like more information on these Aerospace projects, please visit our registration page or call toll us free 1-855-377-6821.
LONG-TERM TESTING Aerospace company needs materials laboratory for testing new aircraft part including mechanical property testing for composites and plastics.Our immediate needs are tests for Flexural and Bearing strength of Lamitex Fr-4 Glass/Epoxy material per ASTM D790-15 and ASTM D953-10 accordingly.Tests required to support certification of newly designed aircraft parts.
Polymer laboratory needed for nondestructive NDT Testing: heat resistance testing of an acrylic lens according to IWA MIL-PRF-5425. Also, need physical properties such as elongation, tensile strength testing of O-rings made out of 51+/-5 durometer EP rubber compounds according to E5001B, E1100-50, EA454-50 or chemically equivalent.
Electrical laboratory needed for SAE compliance testing of optical warning devices used on authorized emergency, maintenance, and service vehicles to SAE J845 Class 1 . Recommended practice providing design guidelines, test procedures, and performance requirements for 360 degree optical warning devices and selective coverage defined as any light that provides greater coverage then 40 degrees left-to-right but less than 360 degrees. Intended for authorized emergency, maintenance and service vehicles. Lighting tested from 5 degrees upward to 5 degrees downward.
Materials Laboratory needed for Corrosion testing of molybdenum disulfide according to AMS-M-7866A. Tests required are:
1.Corrosion resistance in accordance with MIL-STD-791
2.Steel and copper corrosion. Performed on steel panels conforming to MIL-S-7952 and copper panels conforming to QQ-C-576.
Large aerospace company needs laboratory for SAE fuel system testing to 3 SAE Standards: SAE J2260, Non-metallic Fuel System Tubing with One or More Layers, SAE J2044 Quick Connect Coupling Specification for Liquid Fuel and Vapor/Emissions Systems and SAE J2045, Performance Requirements for Fuel System Tubing Assemblies
Laboratory needed for multiple tests on Oil Cooling System including crash, vibration, contamination, fire, oil leakage, thermal cycling, etc:
1. Temperature & latitude test as per DO 160 Section 4 Category -B3.
2. Temperature Variation test as per DO 160 D Section 5 Category-A.
3. Fluid Suceptability test as per DO 160 D Section 11 Category-F.
4. Humidity test as per DO 160 D Section 6 Category-C.
5. Fungus test as per DO 160 D Section 13 Category-F.
6. Salt Spray test as per DO 160 D Section 14 Category-S.
7. Water Proofness test as per DO 160 D Section 10 Category-S.
8. Icing test as per DO 160 D Section 24.
9. Operation shocks & crash safety test as per DO 160 D Section 7 Helicopter Category.
10. Constant Acceleration test test as per MIL-STD-810 Method 513.5.
11. Vibration test as per DO 160 D Section 8 Category-R.
12. Fire test as per ISO 2685.
13. Contamination Test as per CS-E-840.
14. Fire test as per ISO 2685.
First 5 minutes testing with air / oil flow simulating engine
running at minimum power rating (condition to be defined )
followed by 10 minutes with no air / oil flow (engine stop
condition) there shall be no oil spillage throughout the test
15. Contamination Test as per CS-E-840.
16. Fungus test as per DO 160 D Section 13 Category-F.
Test Condition :-
This test to be carried out in test chamber where air
temperature 30±1°C and relative humidity _85%. During the
test, OCS shall not be operating.
17. Image 1 for Performance test.
18. Image 2 for pressure drop test.
19. Proof Pressure Test :-
Test conditions : P= 450 kPa,
Temperature Of Oil = 293 ± 10 K (20°C ± 10°C)
20. Ultimate Pressure Test :-
The Oil/ Air Cooler shall be subjected to an Ultimate Pressure
Test in accordance with para 4.3.5.
Test conditions : P = 520 kPa, Temperature Of Oil = 293 ± 10 K
Oil leakage shall be measured and recorded.
21. Cycle Test ( Fatigue) :-
The Oil / Air Cooler shall be subjected to a Pressure Cyclic Test in accordance with the requirements of this specification.
Test conditions : T oil = 393 ± 5 K
Pressure Proof = 0 and 450 kPa
Number of cycles : 100 000
22. Thermal Cycling Test :-
The Unit shall be designed to withstand 10000 thermal cycles at an ambient temperature of
130°C, cooling air temperature of 15°C and Oil temperature as define
Physical Laboratory needed for flammability pre-testing of carbon fibre samples to CS 25.853 Flammability Requirements for Aircraft Seat Cushions Appendix F, Part I, (a)(1)(ii) (i.e. 12sec vertical burn with 305mm x 70mm samples). The objective is to try 2 or 3 different materials to assist material selection and build up some confidence before testing at the lab required by our customer.
Aerospace company needs materials laboratory for investigation study of delamination problem with decor laminating application.by coupled TGA-MS (Thermalgravimetric Analysis and Mass Spectrometry) to detect if offgassing occurs. We often see delamination or air bubbles popping in the interface between decor film and surface of honeycomb sandwich panel. We would like to know if there offgassing of film affecting the strength of adhesive causing delamination/air bubbles. (note: air are entrapped in honeycomb sandwich panels. thus offgassing might occurs when the air escapes from the core to the surface and is brought contact with the adhesive)
LONG TERM TESTING Analytical Chemistry Laboratory needed for periodically quality control testing silica gel prior to procurement of large quantities to strict quality standards.
Material : SILICAL ? SORBEAD ?R?
1. Chemical composition
4. Bead size
5. Pore diameter
6. Pore volume
7. Specific surface area
8. Bulk density
9. Specific Heat
10. Attrition Loss
11. Expected life
12. Crushing Strength
13. Pressure drop
14. Achieved dew point
15. Static Adsorption ar 10%,20%,20%60%,80% RH
16. pH value
17. Reactivation/Regeneration Temperature
18. Water Resistant