|
|
|
Payload
Integration Working Group Meeting
Deceber 2, 1998
Vandenberg Air Force Base,
CA
OPAL Action Item Summary
-
review payloader ICD matrix,
return to OSSS
-
we need to get the switches
for our separation confirmation signal
-
get freq. license, get the info
on it to Buckley
-
post test info on web
-
add beacon specs to ICD for
the after-separation pulse
Notes summary:
JAWSAT
-
integration order: ASU,
OPAL, OCS, Falconsat, MSFC
-
need information from payloaders
on required check-out tests after integration
-
preferable to have payload people
at WSU for integration help
-
payloaders can turn on their
radios for check-out tests at WSU and in EPF at VAFB
-
payloads will be trickle-charged
as long as possible on the pad, possibly up to 1-2 days before launch
Falconsat
-
right now not planning to turn
on if not deployed, but PI trying to change that
OCS
-
orbit data:
alt: 750 km
inc: 100 degrees
RA: 265 degrees
ecc: 0
epoch: Sept. 15, 1999
CSA
-
will need payloader mass models
again in March
-
should have design for SoftRide
in about 3 weeks
Buckley
-
all payloaders and OSSS need
to operate together as "one harmonious organism"
-
OSSS and Buckley to talk about
how to reduce costs -- may not need to meet so often as a group
OSC
-
the 14 g axial and 8.7 g lateral
transient loads are for a 300 lb payload and will be less for the 400 lb
JAWSAT
-
the two shocks in table 1 of
the new loads data are for JAWSAT-4th stage separation -- payloads will
never see this
-
proposed preliminary sep sequence:
ASU, OPAL, OCS, Falconsat, JAWSAT
General
-
possibility of having pre-ship
review at VAFB at end of April, could bring OPAL to meeting, have OSSS
take it back
-
ejection velocities should be
a low as possible, with .5 ft/s being the lowest allowed
-
WSU has frequency allocation
without a license, may launch without the license and let the license catch
up after launch
|