Apollo 16 User Manual

Apollo 16 Hardware Manual Specifications 29
ANALOG I/O
Analog Outputs 1 – 16
Dynamic Range 118.5 dB (A–weighting)
Signal-to-Noise Ratio 118.2 dB (A–weighting)
Total Harmonic Distortion + Noise -107.5 dB @ -1 dBFS
Connector Type Two Female DB25, Tascam wiring
Monitor Outputs 1 – 2
Dynamic Range 115 dB (A–weighting)
Signal-to-Noise Ratio 115 dB (A–weighting)
Total Harmonic Distortion + Noise -105.5 dB @ -1 dBFS
Gain Range (Monitor Knob) -INF to 0 dBFS
Connector Type Two Male Balanced XLR (pin 2 hot)
All Analog Outputs
Frequency Response 20 Hz – 20 kHz, ±0.05 dB
Channel Separation (Crosstalk) -120 dB
Output Impedance 600 Ohms
Stereo Level Balance ±0.01 dB
Gain Settings +4 dBu or -10 dBV (reference level is selectable in pairs)
Max Output Voltage (Reference Level @ +4 dBu, Balanced) 20.2 dBu (18 dBV, 7.94 VRMS, 0 dBFS)
Max Output Voltage (Reference Level @ -10 dBV, Balanced) 14.2 dBu (12 dBV, 3.98 VRMS, 0 dBFS)
Max Output Voltage (Reference Level @ -10 dBV, Single-Ended) 8.2 dBu (6 dBV, 2 VRMS, 0 dBFS)
DIGITAL I/O
AES/EBU
Connector Type XLR
Format IEC 60958 Type I
MADI
Connector Type Dual Optical SC-Plug (ISO/IEC 9314-3)
Format AES10
Supported Modes @ Sample Rates of 88.2 kHz and Higher Standard, Legacy
Word Clock
Connector Type BNC
Lock Range ±0.5% of any supported sample rate
Word Clock Input Termination 75 Ohms, switchable
Syncronization Sources
Internal, Word Clock, AES/EBU
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Apollo 16 Specifications

General

Mission Type	Manned lunar landing
Launch Date	April 16, 1972
Landing Date	April 27, 1972
Launch Vehicle	Saturn V
Crew Size	3
Commander	John W. Young
Command Module Pilot	Thomas K. Mattingly II
Lunar Module Pilot	Charles M. Duke Jr.
Lunar Surface EVA Duration	20 hours, 14 minutes
Total Mission Duration	11 days, 1 hour, 51 minutes
Landing Site	Descartes Highlands
Lunar Stay Time	71 hours, 2 minutes
Lunar EVAs	3
Lunar Module	Orion (LM-11)
Command Module	Casper (CM-113)
Rover Used	Lunar Roving Vehicle
Distance Traveled by Rover	26.7 km (16.6 miles)