Space & Satellite Transducer Series

213-36-860
Amplified, Absolute

0 - 4,060 PSIA

  

This space-qualified, 0 - 4,060 PSIA, high-pressure amplified transducer was designed decades ago for mission critical satellite and space probe missions. From fuel pressure monitoring systems on satellites and space probes to servo-valves and actuators on space vehicles, these space transducers are designed to tolerate high levels of shock and vibration without damage.

With customizable external features such as connector types, pressure port configurations and mounting methods, Paine satellite transducers are well suited for remote applications that require extreme accuracy and long term performance in a small location.

 

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Need something new? If you cannot find a product to match your current and/or future requirements, please contact us today at 509-881-2100.

 

 

 

 

 

Paine Electronics, LLC

5545 Nelpar Drive

East Wenatchee, WA  98802

Telephone: 509-881-2100

Fax: 509-881-2115

moreinfo@paineelectronics.com

 

 

Pressure Data

Pressure Range:0-580 PSIA and 0-4,200 PSIA

(0-40 and 0-280 bar)

Proof pressure:6,091 PSI (420 bar)
Burst pressure:10,153 PSI (700 bar)

Thermal Properties

Operating temperature range:-25°C to +50°C
Compensated temperature range:+16°C to +45°C

Accuracy

Total Error Band Including Nonlinearity, Hysteresis, Repeatability and Thermal Effects: ± 1.5% Full Scale (Best straight line method)

Physical Properties

Pressure media:Any compatible with 15-5 PH Cond. H1025 CRES and Class 304L CRES
Weight:200 grams max

Transducers designated PSIS have sealed reference chambers.

The voltage output is referenced to 14.696 PSIA.

Electrical

Input Voltage:+24.5 to +32 Vdc (28 Vdc nominal), Reverse Voltage Protected
Maximum Power Comsumption:0.74 W at 29.5 Vdc
Output Voltage:0-5 ± 0.05 Vdc
Output Load:> 0.5 Mohms, 100 kohms short circuit protected
Input/output isolation:100 Mohms min at 50 Vdc for 30 seconds

Environmental

Acceleration:20 G's per MIL-STD-810, METHOD 513.1, PROC. I
Vibration:20 G's per MIL-STD-810, METHOD 514.1, PROC. V, PART I
Shock:30 G's per MIL-STD-810, METHOD 516.1, PROC. IV

Error due to combined effect of shock, vibration, and acceleration

shall be less than 0.01% of F.S. per G.

Electrical Connections

Pin A:+ Input
Pin B:+Output
Pin C:- Output
Pin D:- Input
Pin E:Case Ground
PIN F:No Connection

Mates with MS3116-10-6S (Bendix PT06A-10-6S-(SR)) or equivalent.

Our part no. 247-99-100-02. Mating connector not supplied with transducer.

 

 

 

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