Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

ESRO 2B

From Wikipedia, the free encyclopedia
Research satellite

ESRO 2B
Mission typeAstrophysics
OperatorESRO
COSPAR ID1968-041A[1]
SATCATno.03233
Spacecraft properties
Launch mass89.8 kilograms (198 lb)
Start of mission
Launch date17 May 1968, 02:06:00 (1968-05-17UTC02:06Z) UTC[2][1]
RocketScout B
Launch siteVandenbergSLC-5
End of mission
Decay date8 May 1971, shortly after 03:00 UT
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude326 kilometres (203 mi)[2]
Apogee altitude1,086 kilometres (675 mi)[2]
Inclination97.2 degrees[2]
Period98.9 minutes[2]
Epoch16 May 1968, 22:09:00 UTC[3]

ESRO-2B orIris (International Radiation Investigation Satellite; sometimesIris 2[4]) or sometimesESRO II (orESRO 2), was a Europeanastrophysical spin-stabilised researchsatellite which was launched in 1968. Operated by theEuropean Space Research Organisation, ESRO 2B madeastronomical surveys primarily inx-ray andsolar particles detectors.[5]

Spacecraft

[edit]

ESRO-2B was an 89 kg (196 lb) cylindricalspacecraft with a length of 85 cm and a diameter of 76 cm. On 10 December 1968 (approx 195 days since mission start) the on-boardtape recorder suffered a mechanical failure. This effectively ended the two X-ray experiments as they did not provide any significant data return from then on. Other experiments could still be operated through ground radio links.

ESRO-2B was launched on aScout B rocket into ahighly ellipticalnear-polar orbit on 17 May 1968. Its predecessor satellite,ESRO-2A (sometimesIris 1) failed to reach orbit on 29 May 1967,[6] launching on a Scout B rocket fromVandenberg AFB SLC-5. The cause of failure was malfunction of the third stage of the rocket, preventing the satellite from reaching orbit. ESRO-2A was similar to ESRO-2B except it weighed a little less (74 kg).[4]

Spin-stabilised, ESRO-2B had a spin rate of approximately 40rpm and re-entered Earth's atmosphere on 8 May 1971 after completing 16,282 orbits.[4]

Instruments

[edit]

Seven instruments were carried aboard EROS 2B[2] designed to detect high energy cosmic rays, determine the total flux of solar X-rays and to measureVan Allen belt protons andcosmic ray protons.[5] While designed for solar observations ESRO-2B is credited with the detection of X-rays from non-solar sources.[2] The instruments were:

  • Monitor of Energetic Particle Flux
  • Solar and Van Allen Belt Protons
  • Solar and Galactic Alpha Particles and Protons
  • Primary Cosmic Ray Electrons
  • Hard Solar X-rays
  • Soft Solar X-rays
  • Flux and Energy Spectra of Solar and Galactic Cosmic Ray Particles

References

[edit]
  1. ^ab"NASA – NSSDCA – Spacecraft – Details".
  2. ^abcdefg"ESRO 2B".NASA. Retrieved6 March 2013.
  3. ^"NASA – NSSDCA – Spacecraft – Trajectory Details".nssdc.gsfc.nasa.gov. Retrieved1 May 2018.
  4. ^abc"ESRO 2A, 2B (Iris 1, 2)". Gunters Space Page. Retrieved6 March 2013.
  5. ^ab"ESRO 2B: May – December 1968". University of Indiana. Retrieved6 March 2013.
  6. ^"NASA – NSSDCA – Spacecraft – Details".
Retrieved from "https://en.wikipedia.org/w/index.php?title=ESRO_2B&oldid=1211980064"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp