over operating free-air temperature range (unless otherwise noted)(1) | MIN | NOM | MAX | UNIT |
|---|
| ELECTRICAL |
| VCC | Supply voltage for LVCMOS core logic (2)(3) | 3.0 | 3.3 | 3.6 | V |
| VCCI | Supply voltage for LVDS receivers (2) (3) | 3.0 | 3.3 | 3.6 | V |
| VCC2 | Mirror electrode and HVCMOS supply voltage (2) (3) | 8.25 | 8.5 | 8.75 | V |
| VMBRST | Clocking pulse waveform voltage applied to MBRST[15:0] input pins (supplied by DLPA200) | –27 | | 26.5 | V |
| MECHANICAL | | | | | |
| Static load applied to electrical interface area, see (4) Figure 6-5 | | | 1334 | N |
| Static load applied to the thermal interface area, see (5) Figure 6-5 | | | 156 | N |
| Static load applied to Datum 'A' interface area Figure 6-5 | | | 712 | N |
| ENVIRONMENTAL (6) |
| Illumination power density (4) (12) | < 363nm (7) | | | 2 | mW/cm2 |
| 363 to 400nm(8) | | | 5.2 | W/cm2 |
| | 12.5 | W |
| 400 to 420nm(8) | | | 11 | W/cm2 |
| | 26.6 | W |
| 363 to 420nm total (8)(9) | | | 11 | W/cm2 |
| | 26.6 | W |
| > 420nm | Thermally limited (8) | W/cm2 |
| TC | Case/array temperature (10)(11) | 20 | | 30 (12) | °C |
| TGRADIENT | Device temperature gradient – operational (13) | | | 10 | °C |
| RH | Relative humidity (non-condensing)(14) | | | 95 | %RH |
| Operating landed duty cycle (15) | | 25% | | |
(1) The functional performance of the device specified in this
data sheet is achieved when operating the device within the limits defined by
the Recommended Operating Conditions. No level of performance is implied when
operating the device above or below the Recommended Operating Conditions limits.
(2) All voltages referenced to VSS (ground).
(3) Voltages VCC, VCC2, and VCCI, are required for proper DMD
operation. VSS must also be connected.
(4) Load should be uniformly distributed across the entire
electrical interface area.
(5) Load should be uniformly distributed across the thermal
interface area. Refer to
Figure 6-5.
(6) Optimal, long-term performance and optical efficiency of the
Digital Micromirror Device (DMD) can be affected by various application
parameters, including illumination spectrum, illumination power density,
micromirror landed duty-cycle, ambient temperature (storage and operating), DMD
temperature, ambient humidity (storage and operating), and power on or off duty
cycle. TI recommends that application-specific effects be considered as early as
possible in the design cycle.
(7) The maximum operating conditions for operating temperature
and illumination power density for wavelengths < 363nm should not be
implemented simultaneously.
(8) Also limited by the resulting micromirror array temperature.
Refer to Case Temperature and Micromirror Array Temperature Calculation for
information related to calculating the micromirror array temperature.
(9) The total integrated illumination power density from 363 to
420nm shall not exceed 11 W/cm2 (or 26.6 W evenly distributed on the active
array area). Therefore if 2.5 W/cm2 of illumination is used in the 363 to 400nm
range, then illumination in the 400 to 420nm range must be limited to 8.5 W/cm2
.
(10) In some applications, the total DMD heat load can be
dominated by the amount of incident light energy absorbed. See Micromirror Array
Temperature Calculation for further details.
(11) Temperature is the highest measured value of any test point
shown in Figure 18 or the active array as calculated by the Micromirror Array
Temperature Calculation.
(12) See the Micromirror Array Temperature Calculation for
thermal test point locations, package thermal resistance, and device temperature
calculation.
(13) As either measured, predicted, or both between any two
points - measured on the exterior of the package, or as predicted at any point
inside the micromirror array cavity. Refer to Case Temperature and Micromirror
Array Temperature Calculation.
(14) Various application parameters can affect the optimal,
long-term performance of the DMD, including illumination spectrum, illumination
power density, micromirror landed duty cycle, ambient temperature (both storage
and operating), case temperature, and power-on or power-off duty cycle. TI
recommends that application-specific effects be considered as early as possible
in the design cycle. Contact your local TI representative for additional
information related to optimizing the DMD performance.
(15) Landed duty cycle refers to the percentage of time an
individual micromirror spends landed in one state (12° or –12°) versus the other
state (–12° or 12°).