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930625.DFC" (28226 bytes) was created on 06-25-93
5-Jun-93 Daily File Collection
These files were added or updated between 24-Jun-93 at 21:00:00 {Central}
and 25-Jun-93 at 21:01:14.
--=--=START=--=--= NASA Spacelink File Name:930625.REL
/25/93: NATIONAL AERO-SPACE PLANE TECH TRANSFER EXHIBIT AT NASA
rucella Andersen
eadquarters, Washington, D.C. June 25, 1993
DITORS NOTE: N93-36
Media representatives are invited to view an exhibit of technology
ransfer "success stories" involving the National Aero-Space Plane (NASP)
rogram on Monday, June 28.
The exhibit will be open from 11 a.m. until 4 p.m. EDT in the west lobby
f the NASA Headquarters building at 300 E Street, S.W., Washington, D.C. NASP
fficials will be on hand to discuss technology transfer results that benefit a
ide range of American business, including the aircraft, automotive and medical
ndustries.
end -
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:930625.SHU
SC SHUTTLE STATUS REPORT 6/25/93
STS-51 SPACE SHUTTLE STATUS REPORT
Friday, June 25, 1993
eorge H. Diller
ennedy Space Center
ehicle: OV-103/Discovery Mission number: STS-51
ocation: VAB High Bay 1 Orbital altitude: 184 sm
rimary payload: ACTS-TOS/ORFEUS-SPAS Inclination: 28.45 deg
aunch timeframe: NET July 17 Landing site: KSC
ission duration: 9 + 1 days Crew size: 5
TS-51 IN WORK:
installing ACTS-TOS/ORFEUS-SPAS into payload changeout room
Shuttle Interface Test (mechanical portion) in VAB
removal of VAB access platforms
positioning crawler transporter beneath MLP in High Bay 1
TS-51 WORK SCHEDULED:
Space Shuttle rollout from VAB to Pad B at 12:30 a.m.
Space Shuttle hard-down on launcher pedestals 7 a.m. Saturday
move rotating service structure Saturday
power-up Discovery Saturday
crew hatch functional check Saturday
installation of payloads into Discovery Sunday
mate orbiter mid-body umbilical unit (OMBUU) Sunday
ORK SCHEDULED continued
Flight Readiness Test Monday
ORFEUS-SPAS argon servicing Monday
KSC Launch Readiness Review Monday
astronaut arrival for TCDT and safety training Monday 7 p.m.
ACTS-TOS Interface Verification Test with Discovery Tuesday
ACTS Functional Test Wednesday
ACTS battery charging Wednesday
TCDT begins Wednesday 8 a.m.
TCDT concludes Thursday 11 a.m.
STS-51 Flight Readiness Review Thursday
helium signature test Friday
inertial measurement unit calibration Friday
ORFEUS-SPAS IVT Saturday, July 3
TS-51 WORK COMPLETED:
installation of main engine heat shields
Shuttle Interface Test (electrical portion)
hydraulic testing of solid rocket booster control systems
main engine/main propulsion system interface leak checks
external tank/orbiter interface leak checks
payload arrival at Pad 39-B (1 a.m. today)
PECIAL TOPICS: STS-57 KSC Landing Times on Tuesday, June 29
7:08 a.m. EDT
8:46 a.m. EDT
0:25 a.m. EDT
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:930625.SKD
aily News/TV Sked 6-25-93
aily News
riday, June 25, 1993 Two Independence Square, Washington, D.C..
udio Service: 202/358-3014
% EURECA retrieved;
% Landsat-4 and 5 results;
% Administrator Goldin announces appointments;
% National Space Club speech to air today.
* * * * * * * * * * * * * * *
ndeavour's crew captured and stowed the EURECA satellite at 12:36 p.m. EDT
esterday. The European Retrievable Carrier's two solar panels retracted and
atched into place as planned. However, EURECA ground controllers were unable
o get the two radio antennas completely into position for a positive latch
ndication.
stronauts Low and Wisoff will do an extravehicular activity today to continue
ecuring the EURECA satellite in the cargo bay.
* * * * * * * * * * * * * * *
he Landsat-4 and-5 data presented at the press briefing yesterday regarding
ropical deforestation and adverse effects on tropical forest habitat indicates
hat in the period between 1978-88, the extent of deforestation in the
razilian Amazon Basin was less than expected. However, deforestation did
ncrease substantially and created adverse "edge effects" that pose a
ubstantial threat to the habitat of plant and animal species.
he study shows that during the period, the rate of deforestation in the
razilian Amazon Basin was 6,000 square mile (15,000 square kilometers) per
ear. The results from this study, which was conducted by the Goddard Space
light Center and the University of New Hampshire, is published in today's
ssue of Science magazine.
* * * * * * * * * * * * * * *
ASA Administrator Daniel S. Goldin announced yesterday the appointment of two
stronauts to senior management positions at NASA Headquarters.
illiam M. Shepherd and James D. Wetherbee will serve as Assistant Deputy
dministrators - Technical. They will assist the Administrator and the Acting
eputy Administrator by providing technical oversight of NASA's programs.
n this capacity, Shepherd and Wetherbee also will act as leaders of the
ransition activities for the Redesign Space Station program under the
irection of Bryan O'Connor, Director, Space Station Redesign.
* * * * * * * * * * * * * * *
ASA Administrator Goldin's speech to the National Space Club will air today at
:00 pm EDT. The speech was taped on June 23, 1993 in Crystal City, VA. The
peech will air again on Monday, June 28, 1993 at 11:30 am EDT.
* * * * * * * * * * * * * * *
Here's the broadcast schedule for Public Affairs events on NASA TV.
ote that all events and times may change without notice and that all times
isted are Eastern. Live indicates a program is transmitted live.
riday, June 25, 1993
ive 1:00 pm STS-57 Mission Update
ive 3:30 pm STS-57 Mission Status Briefing
aped 4:00 pm NASA Administrator Daniel Goldin's Speech to the
National Space Club. (Taped on June 23, 1993)
7:30 pm Replay of Flight Day 5 activities.
aturday, June 26, 1993
ive 9:00 am STS-57 Mission Status Briefing
ive noon STS-57 Mission Update
7:30 pm Replay of Flight Day 6 activities
ASA TV is carried on GE Satcom F2R, transponder 13, C-Band, 72 degrees West
ongitude, transponder frequency is 3960 MHz, audio subcarrier is 6.8 MHz,
olarization is vertical.
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_12_7.TXT
ir element set #149 (25-Jun-93)
ir
16609U 86 17 A 93176.45525107 .00002667 00000-0 37514-4 0 1491
16609 51.6178 177.9787 0005686 127.6369 232.5158 15.58489201420428
atellite: Mir
atalog number: 16609
poch time: 93176.45525107
lement set: 149
nclination: 51.6178 deg
A of node: 177.9787 deg Semi-major axis: 3655.5741 n.mi.
ccentricity: 0.0005686 Apogee altitude: 213.7186 n.mi.
rg of perigee: 127.6369 deg Perigee altitude: 209.5614 n.mi.
ean anomaly: 232.5158 deg Altitude decay: 0.0042 n.mi./day
ean motion: 15.58489201 rev/day Apsidal rotation: 3.7455 deg/day
ecay rate: 2.6670E-05 rev/day~2 Nodal regression: -5.0141 deg/day
poch rev: 42042 Nodal period: 92.3355 min
hecksum: 334
.L.CARMAN
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_45_11_10.TXT
CC Status Report #8
ISSION CONTROL CENTER
TS-57 Status Report #8
CORRECTED 4 P.M. CDT)
hursday, June 24, 1993, 3:30 p.m. CDT
ndeavour's crew captured and stowed the EURECA satellite at 11:36 a.m. CDT
oday when the payload retention latches and keel latch locked down onto the
pecial berthing platform in the aft cargo bay.
he European Retrievable Carrier's two solar panels retracted and latched into
lace as planned. But, EURECA ground controllers could not get the two radio
ntennas completely into position for a positive latch indication. The number
ne antenna was about four degrees from complete retraction and the number two
ntenna was two degrees from its stowed position. After an additional attempt
o drive both latch motors in the primary and redundant modes, payload
ontrollers and the Mission Control team decided to berth the satellite with
he antennas unlatched. The remotely operated electrical umbilical was locked
nto place at 11:42 a.m. CDT. The umbilical supplies electricity from
ndeavour's fuel cells to the EURECA satellite's thermal control units to keep
nstrument temperatures at the proper levels.
he EURECA payload controllers and Mission Control teams are refining three
ptions to latch down the two EURECA antennas. The first option calls for the
wo spacewalking astronauts, David Low and Jeff Wisoff, to manually hold down
he antenna booms while EURECA controllers send computer commands to drive the
atches closed. The second option would have the astronauts tie down the
ntenna booms to the main satellite structure. The third option has the
pacewalkers removing the two antennas from the satellite and stowing them
nside Endeavour's crew cabin at the end of the spacewalk.
uring the crew's sleep period tonight, the Planning Team will refine the
etails of the three options for a final decision before the spacewalk begins
t 8 a.m. CDT Friday.
anice Voss wrapped up the Spacehab module experiments for Thursday a few
inutes after 2 p.m. CDT.
ndeavour circles the Earth every 94 minutes in a near-circular orbit with a
igh point of 260 nautical miles and a low point of 255 nautical miles.
-end--
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_45_11_11.TXT
CC Status Report #9
ISSION CONTROL CENTER
TS-57 Status Report #9
riday, June 25, 1993, 5 a.m. CDT
reparations for a space walk planned to start at 8:02 a.m. central time today
ave been progressing smoothly aboard Endeavour.
stronauts David Low and Jeff Wisoff will spend about 40 minutes of their five
ours outside working to secure two antennas on the European Retrievable
arrier satellite retrieved by the shuttle yesterday. Remote commands during
he retrieval to retract the antennas did not fold them fully, against the
URECA satellite. Standing on a platform at the end of the shuttle's robot
rm, Low will push each antenna to the fully folded position so that latches
an be remotely closed to hold them secure during Endeavour's return to Earth.
f the latches won't close, then the space walkers will lash the antennas in
lace with straps carried aboard Endeavour.
fter the antennas are secured, the remaining four hours of space walking will
e spent as planned prior to the flight. Low and Wisoff will perform
valuations of moving and aligning large objects while standing at the end of
ndeavour's robot arm, evaluate how well a space walker must be restrained to
erform work such as tightening a bolt, and evaluate general mobility.
uring the space walk, Mission Specialist Nancy Sherlock will control
ndeavour's mechanical arm from the aft cockpit. Low and Wisoff began
reathing pure oxygen inside their spacesuits four hours before the spacewalk,
urging nitrogen from their bodies to prevent a condition commonly called the
ends. Upcoming activities include the beginning of depressurizing Endeavour's
irlock about 7:42 a.m. central; the EURECA antenna securing to start at about
:57 a.m.; and the conclusion of the space walk about 1:02 p.m.
he crew was awakened at 12:07 a.m. central today by the Dire Straits' song
Walk of Life," played by Mission Control in honor of the upcoming space walk.
arly this morning, Commander Ron Grabe fired Endeavour's large orbital
aneuvering system engines to drop the low point of the shuttle's orbit by
bout 45 nautical miles and enhance the landing opportunities that will be
vailable at the end of the mission. Endeavour is now in an orbit with a high
oint of 256 nautical miles and a low point of 210 nautical miles, circling
arth each 93 minutes.
-end--
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_45_11_12.TXT
TS-57 Status Report #10
ission Control Center
TS-57 Status Report #10
riday, June 25, 1993, 4:30 p.m. CDT
he European Retrievable Carrier's dual antennas are safely latched against the
cience satellite following a spacewalk by Mission Specialists David Low and
eff Wisoff.
t the beginning of the five-hour, 50-minute extravehicular activity, David Low
ounted an foot restraint on the end of Endeavour's robotic arm. Mission
pecialist Nancy Sherlock then positioned the arm so Low could gently push the
rms against EURECA's latch mechanisms. Payload controllers then drove the
atches to secure each antenna.
ollowing the EURECA work, Low and Wisoff performed several procedures for an
bbreviated EVA Detailed Test Objective. Activities associated with each of the
reas of investigation -- mass handling, mass fine alignment and high torque --
ere completed with both EVA crewmen taking turns on the robot arm. Low and
isoff wrapped up their spacewalk and returned to Endeavour's airlock shortly
efore 3 p.m. Central.
he STS-57 crew will end their fifth day in space with an eight-hour sleep
eriod, beginning at 4:37 p.m. Central.
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_45_2.TXT
TS-57 KEPLERIAN ORBITAL ELEMENTS
PACELINK NOTE: Spacelink contains an IBM MS-DOS/Windows program (V2L9322.ZIP)
hat will convert M-50 state vectors into the 2-line format preferred by many
allers. Enter IBM at the GO TO prompt and check out the section on satellite
racking programs. This program may prove useful on occasions when the M-50
lements are more current than the 2-line elements.
TS-57 element set GSFC-016 (orbit 65)
TS-57
22684U 93 37 A 93176.68906947 0.00002570 00000-0 47340-4 0 165
22684 28.4593 284.8771 0061514 41.4091 319.1150 15.44254393 659
atellite: STS-57
atalog number: 22684
poch time: 93176.68906947 (25 JUN 93 16:32:15.60 UTC)
lement set: GSFC-016
nclination: 28.4593 deg
A of node: 284.8771 deg Space Shuttle Flight STS-57
ccentricity: 0.0061514 Keplerian Elements
rg of perigee: 41.4091 deg
ean anomaly: 319.1150 deg
ean motion: 15.44254393 rev/day Semi-major Axis: 6811.7019 Km
ecay rate: 0.26E-04 rev/day*2 Apogee Alt: 475.22 Km
poch rev: 65 Perigee Alt: 391.41 Km
OTE - This element set is based on NORAD element set # 016.
The spacecraft has been propagated to the next ascending
node, and the orbit number has been adjusted to bring it
into agreement with the NASA numbering convention.
.A. Parise, Goddard Space Flight Center
.L.CARMAN
STS-57
FLIGHT DAY 5 STATE VECTOR
ON ORBIT OPERATIONS
(Posted 06/25/93 by Don Pearson)
he following vector for the flight of STS-57 is provided by NASA
ohnson Space Center, Flight Design and Dynamics Division for use in
round track plotting programs.
huttle (and Eureca!!!) state vector:
ift off Time : 1993/172/14:49:59.981
ift off Date : 04/26/93
ector Time (GMT) : 123/13:07:21.953
ector Time (MET) : 004/08:52:38.047
rbit Count : 68
eight : 240896.0 LBS
rag Coefficient : 2.00
rag Area : 1208.5 SQ FT
M50 Elements Keplerian Elements
---------------------- --------------------------
= -7873260.5 FT A = 3681.3547 NM
= 20966899.5 FT E = 0.005599
= -1619438.8 FT I (M50) = 28.23583 DEG
dot = -20402.430078 FT/S Wp (M50) = 54.82433 DEG
dot = -8456.006476 FT/S RAAN (M50) = 282.84314 DEG
dot = -11691.380161 FT/S / N (True) = 133.94403 DEG
Anomalies \ M (Mean) = 133.48073 DEG
Ha = 256.763 NM
Hp = 208.967 NM
ean of 1950 (M50) : Inertial, right-handed Cartesian system whose
oordinate System origin is the center of the earth. The epoch
is the beginning of the Besselian year 1950.
X axis: Mean vernal equinox of epoch
Z axis: Earth's mean rotational axis of epoch
Y axis: Completes right-hand system
: Semi-major axis
: Eccentricity N: True anomaly
: Inclination M: Mean anomaly
p: Argument of perigee Ha: Height of apogee
AAN: Right ascension of ascending node Hp: Height of perigee
uestions regarding these postings may be addressed to Roger Simpson,
ail Code DM4, L. B. J. Space Center, Houston, Texas 77058,
elephone (713) 483-1928.
ear Customer, we are in the process of reviewing the contents of
his product and are interested in determining if it fits your needs.
f you use these state vectors, please drop us a postcard and
et us know what we can do to improve your use of this product.
OSTED BY DPEARSON AT VMSPFHOU ON VMSPFHOU.VMBOARDS:PAONEWS
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_45_6.TXT
TS-57 TV SKED, REV K
**********************************************************************
NASA SELECT TV SCHEDULE
STS-57
6/25/93
REV K
**********************************************************************
ASA Select programming can be accessed through GE Satcom F2R,
ransponder 13. The frequency is 3960 MHz with an orbital position
f 72 degrees West Longitude. This is a full transponder service
nd will be operational 24 hours a day.
wo hour edited programs of each flight day will be replayed for Hawaii
nd Alaska on Telstar 301, transponder 9, channel 18. The orbital
osition is 96 degrees West Longitude, with a frequency of 4060 MHz.
udio is on 6.2 & 6.8 MHz. The programs will begin on launch day and
ontinue through landing airing at 11:01PM Central Time.
his NASA Select Television Schedule of mission coverage is available
n COMSTORE, the mission TV schedule computer bulletin board service.
all 713/483-5817, and follow the prompts to access this service.
OTE: The STS-57 launch occurred on Monday, June 21st at 8:07AM CDT
Denotes changes from last revision.
-------------------------- Friday, June 25 ---------------------------
FD5
RBIT SUBJECT SITE MET CDT
---- ------- ---- --- ---
0 * REPLAY OF FD5 ACTIVITIES JSC 04/11:53 08:00 PM
-------------------------- Saturday, June 26 -------------------------
FD6
NOTE: ADDITIONAL SPACEHAB ACTIVITIES MAY BE DOWNLINKED
THROUGHOUT THE DAY.
3 * CREW WAKE UP 04/17:00 01:07 AM
5 P/TV02 EFE ACTIVITIES TDRE 04/19:50 03:57 AM
T=10:00
6 P/TV02 EFE ACTIVITIES TDRW 21:45 05:52 AM
T=15:00 (May not have Ku coverage)
8 MISSION STATUS BRIEFING JSC 04/23:53 08:00 AM
8 P/TV08 FARE TEST #5 DOWNLINK TDRW 05/00:00 08:07 AM
OPPORTUNITY (May be pre-empted
by MSB)
T=19:00
8 P/TV02 LEMZ-3 ACTIVITIES TDRW 05/01:03 09:10 AM
T=5:00
9 MISSION UPDATE JSC 05/02:53 11:00 AM
0 * P/TV06 CNN INTERVIEW TDRW 05/04:15 12:22 PM
T=15:00
2 * CREW SLEEP 05/07:30 03:37 PM
4 REPLAY OF FD6 ACTIVITIES JSC 05/10:23 06:30 PM
7 * CREW WAKE UP 05/15:30 11:37 PM
------------------------- Sunday, June 27 ----------------------------
FD7
NOTE: ADDITIONAL SPACEHAB ACTIVITIES MAY BE DOWNLINKED
THROUGHOUT THE DAY.
0 P/TV02 EFE ACTIVITIES TDRE 05/19:00 03:07 AM
T=15:00
2 MISSION STATUS BRIEFING JSC 05/23:53 08:00 AM
2 P/TV02 LEMZ-4 ACTIVITIES TDRE 06/00:00 08:07 AM
T=5:00
5 MISSION UPDATE JSC 06/03:53 12:00 PM
7 * CREW SLEEP 06/06:30 02:37 PM
9 REPLAY OF FD7 ACTIVITIES JSC 06/09:23 05:30 PM
02 * CREW WAKE UP 06/14:30 10:37 PM
------------------------- Monday, June 28 ----------------------------
FD8
NOTE: SPACEHAB ACTIVITIES MAY BE DOWNLINKED THROUGOUT THE DAY.
07 CREW CONFERENCE TDRW 06/22:00 06:07 AM
T=20:00
08 MISSION STATUS BRIEFING JSC 06/23:53 08:00 AM
10 Ku BAND STOW 07/02:20 10:27 AM
(Not televised)
10 REPLAY OF NASA ADMINSITRATOR JSC 07/02:23 10:30 AM
ADDRESS
T=35:00
10 MISSION UPDATE JSC 07/03:53 12:00 PM
12 * CREW SLEEP 07/06:00 02:07 PM
14 REPLAY OF FD8 ACTIVITIES JSC 07/09:23 05:30 PM
17 * CREW WAKE UP 07/14:00 10:07 PM
--------------------------- Tuesday, June 29 -------------------------
FD9
22 * DEORBIT BURN (Not Televised) 07/22:32 06:39 AM
23 * LANDING KSC 07/23:39 07:46 AM
POST LANDING PRESS CONFERENCE KSC L+TBD
LANDING REPLAYS KSC L+TBD
----------------------- DEFINITION OF TERMS ------------------------
DT: Central Daylight Time
FE: Environmental control and life support system
Flight Experiment
URECA: European Retrievable Carrier
ARE: Fluid Acquisition and Resupply Experiment
D: Flight Day
SC: Johnson Space Center
SC: Kennedy Space Center
EMZ: Liquid Encapsulated Melt Zone
ET: Mission elapsed Time. The time which begins at the moment
of launch and is read: Days/Hours:minutes. Launch= 00/00:00
SB: Mission Status Briefing
/TV: Photo/Television Scene
MS: Remote Manipulator System
CG: Solution Crystal Growth
PACEHAB:Commercial module carried in payload bay
TS: Space Transportation System
DRE,W: Tracking and Data Relay Satellite, both East and West
longitudes
DRSS: Tracking and Data Relay Satellite System
=: Time event duration equals
TR: Video Tape Recorder
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=--=START=--=--= NASA Spacelink File Name:6_2_2_46_2.TXT
/25/93: STS-51 PAYLOADS ARRIVE AT LAUNCH PAD FOR NEXT SHUTTLE LAUNCH
eorge H. Diller June 25, 1993
SC Release No. 70-93
Payloads for the next Space Shuttle mission, STS-51, arrived
t Pad 39-B this morning - passing yet another major milestone in
relaunch processing.
Riding in the payload canister atop the associated
ransporter, the Advanced Communications Technology Satellite
ACTS) and the Orbiting Retrievable Far and Extreme Ultraviolet
pectrometer (ORFEUS) began the 15-mile trip from the Vertical
rocessing Facility (VPF) in the KSC Industrial Area at 9 p.m.
ast night. By 1 a.m. this morning, the payloads were at the
ea-side launch pad.
Payload processing team members are busy today installing
he ACTS-TOS and ORFEUS-SPAS into the pad's payload changeout
oom.
ACTS will serve as a test bed for advanced experimental
ommunications satellite concepts and technology. Its Transfer
rbit Stage (TOS) upper stage booster will lift the satellite to
eosynchronous altitude on the first day of the mission.
ORFEUS is a telescope system which will provide information
n how stars are born and how they die, while also studying
aseous interstellar clouds. Its carrier, the Shuttle Pallet
atellite (SPAS), will be deployed from the orbiter for 40 to 60
ours to allow observations during the flight before being
eturned to the payload bay.
Based on a 12:30 a.m. rollout of the Space Shuttle Discovery
o the pad, the two STS-51 primary payloads are scheduled to be
nstalled into the payload bay on Sunday, June 27.
In upcoming payload milestones, an Interface Verification
est (IVT) is scheduled for Tuesday, June 29, to verify
onnections between ACTS-TOS and Discovery's flight deck as well
s the orbiter's electrical and communications systems. The next
ay, Wednesday, June 30, a functional test is scheduled to verify
he state of health of the ACTS onboard systems. Finally, the
VT for ORFEUS-SPAS will be performed on Saturday, July 3, to
erify electrical connections between the payload and orbiter.
Launch of STS-51 remains targeted for mid-July with an
fficial date to be determined on July 1 at the Flight Readiness
eview.
# # #
Payload Test and Activity Sheet
STS-51 - ACTS-TOS/ORFEUS-SPAS
June 25, 1993
eorge H. Diller
ennedy Space Center
CTIVITY SCHEDULED:
ad 39-B
/25 ORFEUS-SPAS state-of-health check
/27 ACTS-TOS/ORFEUS-SPAS payload bay installation
/28 ORFEUS-SPAS argon servicing
/29 ACTS-TOS IVT
/29 ACTS battery charging
/30 ACTS Functional Test
/03 ORFEUS-SPAS IVT
/11 ACTS-TOS final ordnance operations
/15 Payload bay doors closed for flight
CTIVITY COMPLETED:
angar AO
/11 ACTS arrival at Hangar AO
/16 ACTS spacecraft checkout begins
/25 Systems Electrical Performance Evaluation Test (SEPET)
/03 steerable beam antenna test
/05 solar array edge illumination test
/06 ACTS spacecraft checkout completed
/08 ACTS moved to PHSF
HSF
/18 ACTS Mission Sequence Test
/28 ACTS fueling
/01 Install apogee kick motor
/08 Install pyrotechnics
/13 ACTS flight mate to TOS
/15 ACTS/TOS integrated Mission Sequence Test
/23 TOS hydrazine fueling
/07 ACTS-TOS moved to Vertical Processing Facility
angar AM
/25 ORFEUS-SPAS arrival at Hangar AM
/10 ORFEUS-SPAS checkout begins
/23 ORFEUS telescope installed
/03 IMAPS telescope installed
/08 ORFEUS-SPAS integrated testing begins
/30 ORFEUS-SPAS integrated testing completed
/11 ORFEUS-SPAS moved to Vertical Processing Facility
PF
/18 ORFEUS-SPAS CITE IVT
/19 ACTS-TOS CITE IVT (completed 5/20)
/20 ACTS Functional Test
/21 ORFEUS-SPAS End-to-End communications test
/21 ACTS-TOS/ORFEUS-SPAS payload canister installation
/24 ACTS-TOS/ORFEUS-SPAS moved to launch pad
/25 ACTS-TOS/ORFEUS-SPAS installed in payload changeout room
# # #
Source:NASA Spacelink Modem:205-895-0028 Internet:192.149.89.61
--=--=-END-=--=--=
--=END OF COLLECTION---COLLECTED 10 FILES---COMPLETED 21:59:31=--=