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Apollo 16 User Manual

Apollo 16
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Apollo 16 Hardware Manual Specifications 28
Specifications
All specifications are typical performance unless otherwise noted, tested under the following conditions: 48 kHz
internal sample rate, 24-bit sample depth, 20 kHz measurement bandwidth, with balanced output.
SYSTEM
I/O Complement
Analog Line Inputs 16
Analog Line Outputs 16
Analog Monitor Outputs Two (one stereo pair)
AES/EBU One stereo input, one stereo output
FireWire 800 (IEEE 1394b) Dual ports
Thunderbolt (via Thunderbolt Option Card, sold separately) Dual ports
Word Clock One input, one output
MADI Optical Ports One input, one output
A/D – D/A Conversion
Supported Sample Rates (kHz) 44.1, 48, 88.2, 96, 176.4, 192
A/D Bits Per Sample 24
Simultaneous A/D conversion 16 channels
Simultaneous D/A conversion 18 channels
Analog Round-Trip Latency 1.1 milliseconds @ 96 kHz sample rate
Analog Round-Trip Latency with up to four serial
UAD Powered Plug-Ins via Console application
1.1 milliseconds @ 96 kHz sample rate
ANALOG I/O
Analog Inputs 1 – 16
Dynamic Range 119 dB (A–weighting)
Signal-to-Noise Ratio 119 dB (A–weighting)
Total Harmonic Distortion + Noise -112 dB @ -1 dBFS
Common-Mode Rejection Ratio -75 dB
Frequency Response 20 Hz – 20 kHz, ±0.05 dB
Channel Separation (Crosstalk) -138 dB
Input Impedance 10 Kilohms
Gain Settings +4 dBu or -10 dBV (reference level is selectable in pairs)
Max Input Voltage (Reference Level @ +4 dBu, Balanced) 20.22 dBu (18 dBV, 7.94 VRMS, 0 dBFS)
Max Input Voltage (Reference Level @ -10 dBV, Balanced) 14.22 dBu (12 dBV, 3.98 VRMS, 0 dBFS)
Max Input Voltage (Reference Level @ -10 dBV, Single-Ended) 8.22 dBu (6 dBV, 2 VRMS, 0 dBFS)
Stereo Level Balance ±0.01 dB
Connector Type Two Female DB25, Tascam wiring
(continued)

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Apollo 16 Specifications

General IconGeneral
Mission TypeManned lunar landing
Launch DateApril 16, 1972
Landing DateApril 27, 1972
Launch VehicleSaturn V
Crew Size3
CommanderJohn W. Young
Command Module PilotThomas K. Mattingly II
Lunar Module PilotCharles M. Duke Jr.
Lunar Surface EVA Duration20 hours, 14 minutes
Total Mission Duration11 days, 1 hour, 51 minutes
Landing SiteDescartes Highlands
Lunar Stay Time71 hours, 2 minutes
Lunar EVAs3
Lunar ModuleOrion (LM-11)
Command ModuleCasper (CM-113)
Rover UsedLunar Roving Vehicle
Distance Traveled by Rover26.7 km (16.6 miles)

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