LUNASCAN
DATE-TIME: 19:35:00 Quad |
Primary Target: None
|
Colongitude: 38.2° Phase: 57.1° Lunation: 610.39 days Illumination: 77.1% |
SYNOPSIS: |
Ephemeris: DE421
Observatory: +37°34' +87°32' Tz: -4h00m
Date: 2014-09-04 19:35:38
Date (TT): 2014-09-04 23:36:47
(J2000) Right Ascension: 19h04m07.24s
(J2000) Declination: -18°14'50.9"
(Date) Right Ascension: 19h04m59.76s
(Date) Declination: -18°13'17.9"
Distance: 363802Km
Apparent diameter: 32.85'
Colongitude: 38.2°
Phase: 57.1°
Lunation: 10.39 days
Illumination: 77.1%
Sub-solar latitude: -1.0°
Libration in Latitude: -05°53'
Libration in Longitude: -04°57'
Position angle: -6.2°
Azimuth +142°11'
Altitude +24°50'
Rise: 16h48m
Transit: 22h03m
Set: 2h17m
Rise azimuth: +112°32'
Transit Altitude: +34°
Set azimuth: +246°28'
=========================
REPORT
I've had issues with the main Lunascan computer rarely but it caused me to
reboot during missions a few times with only a few minutes lost. The Lunascan Quad shows the session starting at about
But then I had to do a last minute routine check of the MADAR room and was
supposed to reset the 1382, and found the system wasn't working. I then
suspicioned a power failure or
PROBLEMS/SOLUTIONS/SUGGESTIONS:
WWV great except when doors are closed. Work on exterior antenna.
LCD panel failure on 40” monitor. Proceed without it until a new one can be purchased.
========================
Mode
Level Records - LIMO
8.21.2014
Trailer, 6x10, United Trailer XLE-610SSA30-S
EQUIPMENT
WIRELESS:
Sennheiser Freeport EM1-A (WWV signal from DX-160)
QUAD PROCESSOR:
Samsung, SCQ-040
RECORDERS:
VHS1 on L2 (Quad), Sony SLV-N55
VHS2 on L2 (VMA/SkyCam IR [B Cam] on Quad Cam 3
position), Phillips DUP3340U
VHS3 on L2 (CabCam, CL-34S-2T 60’ IR, color, Quad
Camera 2 position), Sylvania DA-4HO
VHS4 on L1 EyeCam/FinderCam, ORION VR0212A
DVR1 on L2 (Q Sel), Sony RDR-GX7
DVR2 on L1 [default] (SSI Camera, Quad Cam 4 position), Sony RDR-GX257
MONITORS:
Monitor #1, 13"
Monitor #2, 19" Dynex DX-LCD19-09
Monitor #3, 17" Dell E17GFPc
Monitor #4, 40" LCD Toshiba 40RV525U
QUAD CAMERA POSITIONS:
All camera outputs to Quad SAMSUNG SCQ-041P
Camera 1 mini finders (SC-NVA5’s): A (wide angle eye
cam) & B (9x50 #51611 Celestron finder
w/crosshairs)
Y=video R=power
Camera 2 CabCam cam 1 (color,
SC-NVA5 to Quad), cam 2 (Sony CL-34S-2T, night vision, security, to Lab via
RG59)
Camera 3 LPI (not utilized), VMA or SKYGLOBE graphics,
Camera 4: SSI/C-8.
COMPUTERS:
PC1 System
Dell Intel Pentium 4 processor
2 Gigahertz, 256 meg
C Drive, 40 GB
D Drive, 111 GB
Digital to Analog Converter 1: TEP-100 Elite Pro II
Aperture video recorder DVR2
No graphics used
Feeding Quad Cam Position
4
PC2 System
Compaq Presario sr1218nx computer (1)
Digital to Analog Converter 2; TEP-100 Elite Pro II
VIRTUAL MOON ATLAS or SKYGLOBE graphics
Aperture video recorder VHS2
Feeding Quad Cam Position 3
CAMERAS:
Camera 1
Celestron Neximage Solar
System Imager
SSI or A camera = 2032/5=400x
No Barlow or focal reducer used
delivers simrange of 600 mi and FOV of 400 miles
CCD sensor (Charge Coupled Device)
Type HAD (1/4")
OPTICS, prime focus 5 mm
Active area 3.6mm x 2.7 (4.5 mm diagonal)
Pixel size 5.6 micron, square
VGA resolution (640x480) color ¼” CCD chip
Maximum usable framerate @ 640x480
(uncompressed): 30 fps
#11 yellow written filter
Compression 1420
?-Bit on-chip A/D converter
3 MP
Sensitivity <1 lux
ACOMP Computer
Camera 2
LPI (NOT UTILIZED THIS MISSION)
LPI or B camera = 2032/6=340x
Meade Lunar Planetary Imager
Type HV7131E1 (1/3")
OPTICS, prime focus. 6 mm.
Active area 5.18x3.90 mm (6.5 mm diagonal)
Pixel size 8.0 micron, square
VGA resolution (640x480) color
Max usable framerate @ 640x480
(uncompressed): 36 fps
Compression 1420
8-Bit on-chip A/D converter
1.3 MP
Sensitivity <?lux
BCOMP Computer
Compaq Presario sr1218nx XP Home
2.67 GHZ processor, 760 mb
C Drive 80 GB hard drive
OPTICAL TUBE:
Celestron C-8 SCT 8” optical tube
2032 mm f/l
F10
Resolution at lunar range = 0.68 /
.81086 mi or 4281.36469 feet
(30.19' X 60 = 1811.4" /.68' resol = factor of
2663.82353
2160 miles / 2663.82353 = .81086 mi resolution)0.621 mi/km
1 m = 3.28 ‘
GUIDE COMPUTER
Tech2000, DOB Driver II
CONFIG:
(X) SSI in scope
back
( ) Diagonal and ( ) binoc
viewer. Extended hand control DOB Driver II
SKYCAMS:
CX480-SR40, 40’IR (not used)
Check Monitor, 5"
SCANNER
Aircraft, Radio Shack Pro 90
END OF REPORT