Specifications

Specifications

1. POWER:

AC 100 – 240 V, 50/60 Hz, 16 W

 

 

2. DIMENSIONS (H x W x D)

108.2 mm x 250 mm x 352.6 mm

 

10.82 cm x 25 cm x 35.26 cm

 

 

3. WEIgHT:

9.25 lbs / 4.2 kg

 

 

4. STANDARD TEST CONDITION:

Ambient Temperature: 22 +/- 2%

 

Relative Humidity: 65 +/- 5%

5. INPUT/OUTPUT IMPEDANCE & SENSITIVITY:

(EQ FLAT, UNITY GAIN (ALL GAIN, LEVEL AT CENTER, FADER MAXIMUM), FX OFF, LOAD=100K ohm)

5-1. Input Impedance and Reference Level:

Aux:

20K ohm /-10 dBV +/-0.1 dB (316 mV)

 

 

Line:

20K ohm /-10 dBV +/-0.1 dB (316 mV)

 

 

Phono:

47K ohm /-50 dBV +/-0.1 dB (3.16 mV)

 

 

Mic:

10K ohm /-50 dBV +/-0.1 dB (3.16 mV)

 

 

5-2. Output Impedance and Level:

 

 

 

Rec:

2.2K ohm /-10 dBV (316 mV) +/-2 dB

 

 

Master Unbal:

1K ohm /-10 dBV (316 mV) +/-2 dB

 

 

Master Bal.(Load=600 ohm)

600 ohm /-6 dBm (390 mV) +/-2 dB

 

 

Phones (Load=32 ohm)

33 ohm /-10 dBV (316 mV) +/-2 dB

 

 

6. FREQUENCY RESPONSE: (EQ FLAT, UNITY GAIN, FX OFF, LOAD=100K ohm)

 

 

Line, Aux:

20 Hz – 20 kHz +/-2 dB

 

 

Phono:

20 Hz – 20 kHz +2/-3 dB (RIAA)

 

 

Mic:

20 Hz – 20 kHz +2/-3 dB

 

 

7. THD + N: (EQ FLAT, UNITY GAIN, FX OFF, W/20 kHz LPF, LOAD=100K ohm)

 

 

Line, Aux:

Less than 0.03% @1 kHz

 

 

Phono:

Less than 0.1% @ 1 kHz (A-WEIGHTED)

 

 

Mic:

Less than 0.1% @ 1 kHz (A-WEIGHTED)

 

 

8. MAXIMUM INPUT: (1 kHz, THD=1%, EQ FLAT, UNITY GAIN, FX OFF, LOAD=100K ohm)

 

 

Line, Aux:

More than +14 dBV

 

 

Phono:

More than -26 dBV

 

 

Mic:

More than -26 dBV

 

 

9. MAXIMUM OUTPUT: (1 kHz, THD=1%, EQ FLAT, MAXIMUM GAIN, FX OFF, LOAD=100K ohm)

 

 

Master:

More than +18 dBV (8.0 V)

 

 

Rec:

More than +13 dBV (4.5 V)

 

 

Phones

More than +4 dBV (1.58 V) LOAD=32 ohm

 

 

10. NOISE FLOOR: (EQ FLAT, UNITY GAIN, FX OFF, W/20 kHz LPF, A-WEIGHTED, LOAD=100K ohm)

 

 

Line, Aux:

Less than -86 dBV

 

 

Phono:

Less than -75 dBV

 

 

Mic:

Less than -76 dBV

 

 

11. CROSSTALK: (EQ FLAT, UNITY GAIN, FX OFF, W/20 kHz LPF, A-WEIGHTED, MASTER = +14 dBV OUTPUT)

 

 

L.R Separation:

More than 70 dB @ 1 kHz for LINE, AUX and PHONO

 

 

Between Channels:

More than 86 dB @1 kHz for LINE (AUX) to LINE (AUX),MIC

 

More than 85 dB @ 1 kHz for LINE to PHONO

 

 

12. EQ: (UNITY GAIN, FX OFF, W/20 kHz LPF, LOAD=100K ohm)

 

 

 

Low

10 +/-2 dB, below -32 dB at 70 Hz

Mid

10 +/-2 dB, below -32 dB at 1 kHz

High

10 +/-2 dB, below -32 dB at 13 kHz

 

 

13. CHANNEL BALANCE:

Within 3 dB FROM 0 TO -40 dB

 

 

14. FADER KILL: (EQ FLAT, UNITY GAIN, FX OFF, W/20 kHz LPF, A-WEIGHTED, MASTER = +14 dBV OUTPUT)

 

 

Channel Fader:

More than 85 dB at 1 kHz

 

 

Crossfader:

More than 85 dB at 1 kHz

 

 

15. ACCESSORIES:

 

 

 

User Manual

1 pc

 

 

AC Power Cord

1 pc

 

 

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Page 27
Image 27
Stanton M.207 user manual Specifications, Power

M.207 specifications

The Stanton M.207 is a cutting-edge aircraft designed for multi-role operations, showcasing a synthesis of advanced technologies and innovative features that cater to modern aviation necessities. This aircraft is characterized by a versatile design, enabling it to perform varied missions, including military transport, surveillance, and search and rescue.

One of the standout features of the M.207 is its aerodynamic profile, which contributes to enhanced fuel efficiency and superior flight performance. Its wings are crafted with a high-aspect ratio, providing increased lift and reduced drag, allowing for greater payload capacity without compromising speed or agility. The aircraft’s fuselage is constructed from lightweight composite materials, which not only enhances durability but also contributes to the overall efficiency of the aircraft.

Powering the Stanton M.207 are dual turbofan engines that provide exceptional thrust and allow for impressive operational range and speed. These engines are designed with advanced noise reduction technologies, meeting stringent environmental standards and making the aircraft suitable for operations in noise-sensitive areas. The propulsion system also features an advanced digital engine control system, optimizing performance and fuel consumption in real-time.

In terms of avionics, the M.207 is equipped with a state-of-the-art flight management system (FMS) that integrates various navigation, communication, and surveillance technologies. The cockpit features an advanced glass cockpit layout, enhancing pilot situational awareness and operational efficiency through intuitive displays and controls. The integration of artificial intelligence assists in decision-making processes, significantly improving mission outcomes.

The M.207’s modular design allows for easy configuration adjustments, enabling rapid role changes to suit mission-specific requirements. Whether outfitted for cargo transport, medical evacuation, or reconnaissance missions, the aircraft can be readily adapted without requiring extensive downtime.

Safety is a paramount concern in the design of the Stanton M.207, with multiple redundancy systems incorporated throughout its systems. The aircraft is equipped with advanced collision avoidance systems, enhancing safety during operations in congested airspace. Additionally, the inclusion of an onboard emergency response system ensures that the aircraft can remain operational or safely return to base in the event of failures.

Overall, the Stanton M.207 embodies modern aviation's evolution, merging innovative design with state-of-the-art technologies. Its unique combination of versatility, efficiency, and advanced capabilities positions it as a significant player in the future of multi-role aviation.