Saturday, July 15, 2000

STS-72 (Endeavour)

 1996-001A


The first launch of 1996 was carried out with less publicity than usual because of continuing effects of the government shutdown. Endeavour took off at night, in an unusual launch profile which avoided the need for a single engine TAL abort mode (RTLS and Press to ATO covering the entire ascent). It entered an elliptical 66 x 455 km orbit, and a smaller than usual OMS 2 burn raised the perigee to 180 km.

The EDFT-3 spacewalks made use of an array of ISS EVA equipment stowed in the forward bays. DTO 671 was to evaluate ISS EVAs; DTO 672 tested the electronic cuff checklist, and DTO 833 studied the thermal properties of the improved EMU suit; DTO 1210 covered EVA operations and training. During EVA-1, Chiao and Barray tested the portable work platform and the Rigid Umbilical, as well as foot retsraints. On EVA-2 they practised with connectors and a slidewire, and did force measurements with CLAS, installing the PDAP.


STS-72 
 

DateTimeEventOrbit  

1995 Dec 1  
Roll to VAB 
1995 Dec 4 Mate to ET/SRB 
1995 Dec 6   Roll to LC39B 
1996 Jan 11  0941:00  Launch by Shuttle (STS-72)  
 0943:04  SRB sep 
 0949:28  MECO   
 0949:46  ET sep  66 x 455 x 28.5 
 1024:30  OMS 2 1:11 35.4 m/s 90.94 180 x 460 x 28.5 
 1025:41  OMS 2 CO  
 1057:08  PLBD open 
 1245RCS adjust  
 1500   91.01 186 x 460 x 28.45 
1996 Jan 12  0500   91.00 187 x 460 x 28.45 

0738  RCS burn to avoid MSTI 2  91.04 190 x 460 x 28.45 
  
 1340:02  OMS-3 (L) 2:36 78.0m/s 
 1342:37  OMS-3 CO  
 1430   93.84 458 x 466 x 28.45 
 2200   93.84 458 x 465 x 28.45 
1996 Jan 13  0249:45  Orbit raise OMS-4 (R) NH-S 3m/s 12s  
 0249:58  OMS 4 CO 
 0400   94.01 469 x 472 x 28.45 
 0318?  RCS Phasing burn 1m/s  
 0556:07  RCS NCC 0.4m/s 
 0643:49 RCS TI burn 1m/s 
 0724? MC1 
 0734  MC2 
 0744  MC3 
 0754  MC4 
 0800  Rendezvous with SFU, +Rbar 
 0935  SFU panel 1 ejected 
 0947  SFU panel 2 ejected 
 1057:19  RMS grapple SFU 
 1139:30  RMS berth SFU 
 1150? RMS ungrapple SFU 
 1437:13  OMS-5 Orbit lower 93s 47m/s for OAST 
 1437:47  OMS-5 CO 
 1524:29  OMS-6 Orbit lower 93s 47m/s for OAST 
 1526:02  OMS-6 CO 
 2000   90.67 303 x 311 x 28.45 
1996 Jan 14  0800   90.67 302 x 311 x 28.45 
 1042RMS grapple OAST Flyer 
 1057:13 RMS unberth OAST Flyer 
 1132:33  RMS deploy OAST Flyer 
 1138:30  Sep 1 burn 
 1208  Sep 2 burn 
 2200   90.69 304 x 313 x 28.45 
1996 Jan 15  0525  EVA-1 depress 
 0535  EVA-1 on battery 
 0540  EVA-1 hatch open (Leroy Chiao) 
 0745Leroy Chiao evaluate PWP, 
 0920deploy RU across PLB 
 1005 eval Util Box 
 1132  Ingress, hatch closed 
 1144  Off battery, repress (NASA 6:09:19, JCM 6:19) 
 1230   90.70 303 x 313 x 28.5 
 1450NC3 burn 
 1530   90.60 299 x 309 x 28.5 
 1843RCS NC0 for OAST-flyer phasing  
1996 Jan 16  0500   90.57 292 x 312 x 28.45 
 0631:18  RCS NCC 0.3m/s 
 0728:45  RCS TI 1.5m/s 
 0802MC1 
 0821  MC2 
 0831  MC3 
 0841  MC4 
 0845  Arrive at OAST R-bar, rendezvous  
 0947:15  RMS grapple OAST Flyer 
 1014:02  RMS berth OAST Flyer 
 1015:40  OAST latched 
 1037RMS ungrapple OAST 
 1115   90.65 301 x 310 x 28.45 
1996 Jan 17  0534  EVA-2 depress 
 0540  EVA-2 NASA start 
 0554  Hatch open 
 0635Utility box eval 
 0710PDAP install 
 0752CLAS evaluation 
 0915TERA (Temporary Equpt. Restraint Aid) eval. 
 1020Slidewire and PWP eval 
 1046cold thermal eval of EMU 
 1225  Ingress 
 1234  EVA-2 end (Chiao, Scott) NASA 6:53:41 JCM 7:00 
1996 Jan 18  0600   90.64 301 x 310 x 28.45 
1996 Jan 19  0600   90.64 301 x 310 x 28.45 
1996 Jan 20  0403  PLBD closed 
 0641:23  Deorbit 2:36 82.9 m/s  20 x 310 x 28.5 
 0644:00  OMS DO CO 
 0710:01  Entry  
 0741:41  MGTD KSC RW15 
 0741:43  Drag chute deploy
 0741:51  NGTD 
 0742:47  Wheels stop 
 1120OPF/3 

Friday, July 14, 2000

JAWSAT

 2000-004A


JAWSAT is the Joint Academy-Weber State Satellite. It is amateur satellite Weber Oscar-39 (WO-39). [223] The Weber State (One Stop Satellite Solutions/Ogden) built 64 kg microsat flew on an MSLS (Minuteman) launch vehicle in Jan 2000 under the Orbital-Suborbital Program (OSP). It was built for educational purposes, but will carry some experiments. Originally part of STP, as Space Test Program mission P98-1, it was converted after STP withdrew into a simple Multi-Payload Adapter (MPA).

The orbital MSLS vehicle is called the Minotaur [224] It has the Minuteman 2 stages 1 and 2 with two Pegasus upper stages,. Launch from California Spaceport in S Vandenberg.

The Minotaur has an M55A1 stage 1, an SR-19 stage 2, an Alliant Orion 50XL stage 3, and an Orion 38 stage 4, with a Pegasus fairing. Pegasus fairing is 4.4m long 1.3m dia.

M55A1 is 7.5m long 1.67m dia, 20788 kg prop, 23081 kg full, steel case, TP-H1011 prop. Thrust is 80.7 kN, isp 237s, 60s burn. SR19 is 4.1m long 1.33m dia, 6238 kg prop, 7033 kg full, Ti case, ANB-3066 prop. Thrust is 27 kN, isp 287.5s, 65s burn. Orion 50XL is 3.6m l 1.28m dia, 3915 kg prop, 4332 kgf, GE case, HTPB. Thrust is 15 kN, isp 290.1s, 72s burn. Orion 38 is 1.3ml 1.0m dia, 771 kgp, 897 kgf, GE case, HTPB. Thrust 32 kN, isp 290.2s, 69s burn. (or: 900f 223 em)

JAWSAT consists of the MPA (MultiPayloadAdapter) spaceframe. The PEST and ACP experiments are attached to it, and four subsatellites are ejected. JAWSAT separated from the SRSS (Soft Ride System, 14 kg) and the final stage.

The spacecraft seems to have failed soon after deploying OPAL and OCSE.

Orbit is 700 km polar x 98.4 deg.

The Orbital/Suborbital Program Space Launch Vehicle (OSPSLV) Minotaur launched from the Spaceport Systems International Commercial Launch Facility (California Spaceport.)

The total payload was 126 kg. m1/m2 = 1026 / 349 so dV = 2846 ln m1/m2 = 3069 m/s. Actual burn 2584 m/s?


JAWSAT 
 

DateTimeEventOrbit  

2000 Jan 27  0303 Launch by OSPSLV  V CLF 
  T+1:01 Stage 1 M55A1 sep 33 km 1.51 km/s  -6300 x 70?  
  T+1:20 Stage 2 skirt sep 51 km 1.76 km/s  -6270 x 100? 
  T+1:58 Fairing sep 108 km 2.72 km/s  -6100 x 200? 
  T+2:05 Stage 2 SR19 sep 133 km 2.83 km/s  -6120 x 300 ? 
  T+2:07 Stage 3 burn  
  T+3:20 Stage 3 burnout 
  T+10:04 Stage 3 sep 743 km 
  T+10:15 Stage 4 burn at apogee  -4421 x 734 x 102.3  
 0314 T+11:24 Stage 4 burnout 
  T+12:59 ASUSAT GG boom deploy 
 0316 T+13:14 ASUSAT sep from JAWSAT 
 0316 T+13:44 OPAL sep from J 
 0317 T+14:14 OCSE sep from J 
 0319 T+16:20 Falconsat sep from J 
 0322 T+19:18 JAWSAT sep from St 4 
  T+19:23 CCAM burn 
  T+23:18 CCAM end   
  T+36:40 RCS depletion  750 x 800 x 100.2 

Wednesday, July 12, 2000

Why the Wealthy Give: The Culture of Elite Philanthropy

https://welib.org/md5/80e169cf2cf50e4ad00053bd0050266d

Gals 2

 1995-063A


Gals 2 was launched on 1995 Nov 17 by Proton with a DM-2 upper stage. It had been bought by the Chinese private company Land Group for Asian TV broadcasting and was leased to the Global DBS Company. By 2000 it was back under Intersputnik auspices.


Gals 2 
 

DateTimeEventOrbit  

1995 Nov 17  1425:00  Launch by Proton  KB LC200L 
 1434 Stage 3 sep 
 1530? DM burn 1 
 2050?  DM burn 2 
 2110? DM sep 
1995 Nov 17    1443.09 35799 x 36047 x 0.2 GEO 90.5E 
1995 Nov 19    1441.7 35764 x 36026 x 0.2 88E+1W/d 
1995 Dec 16    1436.30 35780 x 35801 x 0.1 GEO 71.0E 
1996 Jun 11    1436.10 35784 x 35789 x 0.1 GEO 71.0E 
1996 Jun 12   mv out  GEO 70E 
1996 Jul 9   mv in  GEO 36E 
1996 Jul 9    1435.52 35763 x 35787 x 0.0 GEO 35.9E 
1997 Jan 9    1436.08 35777 x 35795 x 0.1 GEO 36.0E 
1999 Oct 17    1436.23 35766 x 35812 x 0.3 GEO 36.6E 

The Arthurian Name Dictionary

 https://welib.org/md5/721666e5aeb5ca1a883b02a8088c5d4a

The Fowlers of Sweet Valley

 https://welib.org/md5/75f955c6bfbec02dc2affc15d49ab5f6

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt