Friday, June 14, 1996

Kosmos 2120

 1990-115A


The Kosmos-2120 mission had an extended 23-day duration and flew in three phases with progressively lower apogees.


Kosmos-2120 
 

DateTimeEventOrbit  

1990 Dec 26  1110:00 Launch by Soyuz  PL 
 1114  Blok-I burn 
 1118  Blok-I sep 
1990 Dec 26    88.54 178 x 225 x 82.6 
1990 Dec 27   
90.34 236 x 346 x 82.6 
1991 Jan 8  90.19 233 x 333 x 82.6 
1991 Jan 11   
89.79 236 x 291 x 82.6 
1991 Jan 15  89.77 235 x 290 x 82.6 
1991 Jan 16  
89.30 228 x 250 x 82.6 
1991 Jan 17    89.25 227 x 248 x 82.6 
1991 Jan 19 Landed after 23d 
 0641?  Deorbit 
 0652? PO sep 
 0700?  Entry  -201 x 245 
 0716? Landed 

The Age of Innocence

 https://www.gutenberg.org/files/541/541.txt

Monday, June 10, 1996

Cluster 1A

 1996-F03


The four Cluster satellites, part of ESA's Cornerstone 1 (CS1) project, were lost in the launch failure of the first Ariane 5.

Cluster F1 was paired with Cluster F2 above the Speltra structure on Ariane 501. The Dornier built satellite had a mass of 1200 kg at launch. 650 kg of this is N2O2/MMH fuel. DDS (Dornier Satellitensysteme) is a unit of Daimler-Benz Aerospace (DASA). The propulsion system was built by Matra Marconi Space/Bristol (formerly British Aerospace) using a DASA 400N/8 x10N thruster system.

The plan was for the Ariane 5 EPS to leave the four spacecraft in a 280 x 36000 km x 10 deg orbit. Cluster F1 and F2 separate from Speltra and then from each other. Five burns with the 400N engine on each satellite leaves them in a 25000 x 140000 km polar orbit. The four spacecraft are maintained in a tetrahedral cluster with 200 to 18000 km separations. The satellite has four 50-m booms with 100m span, and is 2.9m diameter and 1.3m tall. There are also two 5-m booms with magnetometers. Science goals include study of the bow shock, the polar cusp, and the magnetotail. The mission is commanded from ESOC with a science center at RAL.

The Ariane 5 took off from ELA3 at Kourou, but half a minute into the flight, travelling at an altitude of 3500 m, the on-board computer incorrectly read the vehicle's attitude and ordered the vehicle to turn sharply, causing structural failure. The vehicle automatically self destructed when the solid boosters and core stage broke apart.


Cluster F1/Ariane 501 
 

DateTimeEventOrbit  

1996 Jun 4  1233:59  EPC Vulcain ignition (H0) 
 1234:06  EAP ignition  
 1234:06  Launch by Ariane 5 (501)  CSG ELA3 
 1234:36 Altitude 3.5 km  
 1234:36 EAP nozzles hard over 
 1234:37? Vulcain nozzle hard over 
 1234:37  L0+31.3s: EPS N2O4 tank rupture? 
 1234:38.5 L0+32.5s: 90 deg angle of attack 
 1234:38 L0+32.8s? EPC structural breakup 
 1234:39  Vehicle destroyed 

Payload:

  • ASPOC Active SC Potential Control

  • CIS Cluster Ion Spectrometry

  • DWP Digital Wave Processor

  • EFW Electric Fields and Waves

  • EDI Electron Drift Instrument

  • FGM Fluxgate Magnetometer

  • PEACE Plasma Electron and Current Analyser

  • RAPID Research with Adaptive Particle Imaging Detectors

May 13,2026

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