########### P3D IHU-1 Affichage TLM - OE1KIB, OE1VKW -F1HDD -########## A HI, THIS IS AMSAT OSCAR-40 2000-11-26 11:13:44 #007A +--------------------------------------------------------------+ | ALON/ALAT=259/-5, moving to 270/0. D blocks are memory data. | +--------------------------------------------------------------+ ***************************** Orbit data ********************************* Jour AMSAT08365 heure11:13:44.84 TUC Orbite No00021 Phase 034 ***************************** ETAT-- ************************************* RX: U(-1.7dB) L1(0.7dB) TX: V(0x7fW MB) Balises: GB(PSK;) MB(EB source; V) Antennes: #129=0xae Ant/Pre-amps: U-Rx=om U-Tx=hi L-om+preamp Experiment.: IHU-2 Cedex-ctrl Cedex-pwr Batt. prim. on; Charg. on; Compte erreurs memoires: 5 ***************************** Temperatures [øC] ************************** GenSol1 -1.2 GenSol2 15.3 GenSol3 16.0 GenSol4 14.7 GenSol5 14.7 BCR1 8.7 BCR2 15.3 BCR3 13.3 GenSol6 -1.2 BattPriB2 16.0 BattPriB4 16.0 BattPriB6 -1.2 BatAuxB1 9.4 BatAuxB5 11.4 V-TX 31.1 U-Excit 12.0 U-Amp 13.3 S1-TX 14.0 S2-TX 14.0 X-TX 86.0 X-TX TOP 88.1 K-TX -51.2 U&V-RX 16.0 L1-RX 14.7 L2-RX 8.7 S1-HF RX 10.7 S2-C RX 10.7 IHU 4.1 SEU 5.4 EPU 15.3 RF monit -51.2 S ant 14.7 HP1+X-Y 12.7 HP2+X+Y 16.6 HP2+X-Y 16.6 HP2-X 17.9 HP3+X 14.0 HP3-X 14.0 HP4+X+Y 13.3 NH3 B2 16.0 MMH B3 16.6 N2O4-X-Y 16.0 N2O4+X+Y 14.0 He Tank 16.0 Top 24.5 Bottom 9.4 Back 10.7 Side2Pan 12.0 Side4Pan 12.7 ***************************** Voltages [V] ******************************* Batt-Pri 28.7 BattAux 27.3 BCR1-In 22.2 BCR2-In 22.1 BCR3-In 22.9 28V Bus 28.5 10V-C1 BCR2 12.5 10V-C2 BCR3 12.5 ***************************** Courants [mA] ****************************** SP1-BCR1 190 SP4-BCR2 89 SP2-BCR3 291 SP6-BCR1 190 SP5-BCR2 9620 SP3-BCR3 14082 10V-C1 BCR2 363 10V-C2 BCR3 375 28V-S SEU 0x08 28V-Bat 532 28VU1EPU -1 28VU2Bus 6747 28VU3-S 23 28V-BCR 6925 28VS-PA/M 10 10VS-PA/M 0x08 X-Helix 3 K-Tx 0x08 ***************************** Senseurs sol/terre************************** Mode sens. : spin SS1 PLL: locked SS2 count: 7SpinRate[rpm] 5.4 SS Z -25 -20ø SS Y -25 -27øSS Up -X 9ø SS Up -Y 9ø SS Z -45 -34ø SS Y -45 -34øSS Dwn -X 9ø SS Dwn -Y 9ø ***************************** Roues a Inertie **************************** ***************************** Arcjet Motor ******************************* Pression Res. 5Bar Pression Mot. 5Bar Courant Mot. 0.2A Tension Mot. -237.4V Flux 0x08 ***************************** Moteur 400N ******************************** Motor valve: closed High pressure: -167Bar Low pressure: -0Bar **************VERIFICATION CRC************* CALC : CRC=CE47 RECU : CRC=857C Trame : NOK _______________________________________________________________________________ M thorough study of the 70cm Tx problem with the hi-gain ant. 5. The two 2400 MHz transmitters were operated and are ok. 6. Pictures from the separation sequence are being downloaded and will shortly be available on our website. There we will also show the test-schedule for some first amateur operations. 7. Steps after 1st orbit change: test the electric propulsion system and then use it to further increase appogee altitude using the arcjet before the big i-change. --73s Karl-- **************VERIFICATION CRC************* CALC : CRC=CF97 RECU : CRC=CF97 Trame : OK _______________________________________________________________________________ ########### P3D IHU-1 Affichage TLM - OE1KIB, OE1VKW -F1HDD -########## A HI, THIS IS AMSAT OSCAR-40 2000-11-26 11:14:11 #007A +--------------------------------------------------------------+ | ALON/ALAT=259/-5, moving to 270/0. D blocks are memory data. | +--------------------------------------------------------------+ ***************************** Orbit data ********************************* Jour AMSAT08365 heure11:14:11.14 TUC Orbite No00021 Phase 034 ***************************** ETAT-- ************************************* RX: U(-1.3dB) L1(0.7dB) TX: V(0x7fW MB) Balises: GB(PSK;) MB(EB source; V) Antennes: #129=0xae Ant/Pre-amps: U-Rx=om U-Tx=hi L-om+preamp Experiment.: IHU-2 Cedex-ctrl Cedex-pwr Batt. prim. on; Charg. on; Compte erreurs memoires: 5 ***************************** Temperatures [øC] ************************** GenSol1 -1.2 GenSol2 15.3 GenSol3 16.0 GenSol4 14.7 GenSol5 14.7 BCR1 8.7 BCR2 15.3 BCR3 13.3 GenSol6 -1.2 BattPriB2 16.0 BattPriB4 16.0 BattPriB6 -1.2 BatAuxB1 9.4 BatAuxB5 11.4 V-TX 31.1 U-Excit 12.0 U-Amp 13.3 S1-TX 14.0 S2-TX 14.0 X-TX 86.5 X-TX TOP 88.1 K-TX -51.2 U&V-RX 16.0 L1-RX 14.7 L2-RX 8.7 S1-HF RX 10.7 S2-C RX 10.7 IHU 4.1 SEU 5.4 EPU 15.3 RF monit -51.2 S ant 14.7 HP1+X-Y 12.7 HP2+X+Y 16.6 HP2+X-Y 16.6 HP2-X 17.9 HP3+X 14.0 HP3-X 14.0 HP4+X+Y 13.3 NH3 B2 16.0 MMH B3 16.6 N2O4-X-Y 16.0 N2O4+X+Y 14.0 He Tank 16.0 Top 24.5 Bottom 9.4 Back 10.7 Side2Pan 12.0 Side4Pan 12.7 ***************************** Voltages [V] ******************************* Batt-Pri 28.9 BattAux 27.3 BCR1-In 22.7 BCR2-In 22.5 BCR3-In 22.3 28V Bus 28.5 10V-C1 BCR2 12.5 10V-C2 BCR3 12.6 ***************************** Courants [mA] ****************************** SP1-BCR1 190 SP4-BCR2 6274 SP2-BCR3 190 SP6-BCR1 190 SP5-BCR2 12764 SP3-BCR3 7187 10V-C1 BCR2 363 10V-C2 BCR3 350 28V-S SEU 0x08 28V-Bat 1255 28VU1EPU -1 28VU2Bus 6550 28VU3-S 23 28V-BCR 7334 28VS-PA/M 10 10VS-PA/M 0x08 X-Helix 3 K-Tx 0x08 ***************************** Senseurs sol/terre************************** Mode sens. : spin SS1 PLL: locked SS2 count: 7SpinRate[rpm] 5.4 SS Z -25 -20ø SS Y -25 -20øSS Up -X 8ø SS Up -Y 8ø SS Z -45 -34ø SS Y -45 -34øSS Dwn -X 8ø SS Dwn -Y 8ø ***************************** Roues a Inertie **************************** ***************************** Arcjet Motor ******************************* Pression Res. 5Bar Pression Mot. 5Bar Courant Mot. 0.2A Tension Mot. -237.4V Flux 0x08 ***************************** Moteur 400N ******************************** Motor valve: closed High pressure: -167Bar Low pressure: -0Bar **************VERIFICATION CRC************* CALC : CRC=7917 RECU : CRC=7917 Trame : OK _______________________________________________________________________________ ----OE1KIB, OE1VKW -F1HDD --------(c) AMSAT-F 2000-------