PRODERA MODAL ANALYSIS SYSTEMS
AND SOFTWARE

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New products

In-Flight Test Equipment

Vertical Inertial shaker EI 797, Download PDF (369 k)

Horizontal Inertial shaker EI 799, Download PDF (376 k)

Inertial shaker EI 20 for test applications, Download PDF (135 k)

Airbone power amplifier A 520, Download PDF (300 k)

    
Product documentation

Brochure, Download PDF (2 M)

Short description about our products

Why is Modal Analysis so essential, Download PDF (2 Mb) or Download ZIP (900 k)

Turnkey systems for aircraft certification and stores integration, Download PDF (1.87 Mb) or Download ZIP (1 Mb)

Ground Test Equipment

Update of former Prodera systems

PRINUPlt.DLL library for PRIN 80 and PRIN 85, Download PDF (88 k)

Prodera Shakers-Amplifiers general data sheet, Download PDF (294 k)

Catalogue shakers, Download PDF (796 k)

Catalogue amplifiers, Download PDF (606 k)

P-SYS-MODAL / P-WIN-MODAL general information, Download PDF (222 k)

P-SYS-MODAL® detailed description, Download PDF (64 k)

Modal accelerometer, Download PDF (51 k)

8 channel charge amplifier, Download PDF (50 K)

Suspension elastic cords, Download PDF (430 k)

Multipoint air suspension system for aircraft GVT testing, Download PDF (87 k)

Electronic test structure for modal software calibration, Download PDF (35 k)

Detailed presentation of the Electronic Test Structure for modal software calibration Strucsim-3-D® , Download PDF (237 k)

In-Flight Test Equipment

Vertical Inertial shaker EI 797, Download PDF (369 k)

Horizontal Inertial shaker EI 799, Download PDF (376 k)

Inertial shaker EI 20 for test applications, Download PDF (135 k)

Pyrotechnical thrusters firing and synchronisation unit, Download PDF (118 k)

Pyrotechnical thrusters 600 N (134.88 lbf), Download PDF (62 k)

Pyrotechnical thrusters 1800 N (404.64 lbf), Download PDF (50 k)

Flutter prediction software for sub, super and transonic ranges P-FLIGHT-MODAL®, Download PDF (50 k)

    
Related publications

Lecture "Pyrotechnical Equipment for Flutter Investigation"

Presented in Avignon (France) on 18 October 2004 by:

M. Klaas DIJKSTRA – PRODERA

M. Michel PREVOST – ONERA

M. Pierre PREVOT – ONERA

Download PDF (1373 k)

Firing of pyrotechnical thruster, Download (1329 k)

Aircraft modal testing at VZLU, Download PDF (489 k)
Excitation by rotation of forces : Download PDF (489 k)