To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

SACI-1
Mission typeEarth orbiter
OperatorINPE
COSPAR ID1999-057B Edit this at Wikidata
SATCAT no.25941
Spacecraft properties
ManufacturerINPE
Launch mass60 kilograms (130 lb)
Power150 watts
Start of mission
Launch dateOctober 14, 1999 (1999-10-14)
RocketLong March 4B
Launch siteTaiyuan LC-7
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Semi-major axis7,098 kilometres (4,410 mi)
Eccentricity0.00084
Perigee altitude733 kilometres (455 mi)
Apogee altitude745 kilometres (463 mi)
Inclination98.6°
Period99.6 minutes
EpochPlanned
 

The SACI-1 was a microsatellite of scientific applications, designed, developed, constructed and tested by Brazilian technicians, engineers and scientists working in INPE (National Institute of Space Research).[1] SACI-1 was launched on October 14, 1999, from the Taiyuan Satellite Launch Center, China, by means of a Long March 4B rocket, as a secondary payload at the CBERS-1 launch.

YouTube Encyclopedic

  • 1/3
    Views:
    2 232 717
    9 905 767
    685
  • How to Make an Elephant Explode with Science – The Size of Life 2
  • THE MARS UNDERGROUND [HD] Full Movie
  • It's Great To Be a CMU Professional Writing Grad Student

Transcription

Features

The "SACI" satellites are composed of a multi-mission platform and a set of experiments that constitute the payload. These satellites had the cooperation of several Brazilian and foreign institutions.

The SACI-1 scientific satellite has the following characteristics:

  • Format: parallelepiped with 60 cm x 40 cm x 40 cm
  • Mass: 60 kg
  • Orbit: heliosynchronous
  • Stabilization: by rotation (6 rpm)
  • Precision: 1 degree

Energy supply

  • Solar Cells: Gallium Arsenide (AsGa)
  • Dimensions: 3 panels of 57 x 44 cm
  • Efficiency: 19%
  • Power output: 150W
  • Nickel Cadmium (NiCd) Battery Cells
  • Voltage: 1.4 V
  • Capacity: 4.5 Ah
  • Remote control rate: 19.2 kbit/s
  • Transmission rate: 500 kbit/s
  • Antennas of edge: 2 of transmission and 2 of reception, type Microstrip
  • Operating frequency telemetry / remote control: 2,250 GHz / 2,028 GHz
  • Receiving antenna in Soil: 3.4 m in diameter

Mission

Although the launch went smoothly, and the intended orbit reached, SACI-1 did not come into operation, probably due to a failure in the solar panel control system.

References

External links


This page was last edited on 25 April 2024, at 23:46
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.