Dual Air Density Explorer

Explorer (56)
Explorer (56) (DADE-A) satellite
NamesDADE-A
Dual Air Density Explorer-A
DADE-B
Dual Air Density Explorer-B
Mission typeEarth science
OperatorNASA
COSPAR ID1975-DADE-A
Mission durationFailed to orbit
Spacecraft properties
SpacecraftExplorer LVI
Spacecraft typeDual Air Density Explorer
BusDADE
ManufacturerLangley Research Center
Launch mass40 kg (88 lb)
PowerSolar cells and batteries
Start of mission
Launch date6 December 1975,
03:35:01 UTC[1]
RocketScout F-1 (S-196C)
Launch siteVandenberg, SLC-5
ContractorVought
End of mission
DeactivatedFailed to orbit
Orbital parameters
Reference systemGeocentric orbit (planned)
RegimePolar orbit
Perigee altitude350 km (220 mi)
Apogee altitude350 km (220 mi)
Inclination90.10°
Period90.00 minutes
Instruments
Atmospheric Composition Mass Spectrometer
Atmospheric Drag Density

Dual Air Density Explorer was a set of 2 satellites, DADE-A and DADE-B, released as part of NASA's Explorer program. DADE-A and DADE-B was launched on 6 December 1975 at 03:35:01 UTC,[1] by a Scout F-1 launch vehicle from Space Launch Complex 5, Vandenberg Air Force Base, California. The launch of the DADE satellites failed.[2][3]

Spacecraft

The Dual Air Density Explorer-A (DADE-A) satellite was a 76 cm (30 in) rigid sphere designed to determine, in conjunction with Dual Air Density Explorer-B (DADE-B), the vertical structure of the upper thermosphere and the lower exosphere as a function of latitude, season, and local solar time. Both satellites would have been launched by a single Scout launch vehicle into coplanar polar orbits. Measurements of atmospheric density from DADE-A would have been obtained from satellite drag analyses near perigee (approximately 350 km (220 mi)) and from composition measurements taken by an onboard mass spectrometer. DADE-A was equipped with a radio beacon to facilitate tracking.[2]

Experiments

Atmospheric Composition Mass Spectrometer

The mass spectrometer experiment on DADE-A was designed to perform composition measurements in the upper thermosphere (approximately 350 km (220 mi)). The instrument was a magnetic mass spectrometer with a Mattauch-Herzog geometry and would have measured the distribution of such atmospheric constituents as oxygen, nitrogen, helium, hydrogen, neon and argon.[4]

Atmospheric Drag Density

The atmospheric drag density experiment on DADE-A was designed to provide indirect measurements of upper thermospheric density near satellite perigee (approximately 350 km (220 mi)). The experiment had no unique onboard hardware. The density values would have been derived from sequential observations of the satellite's position. The experiment would have yielded systematic values of atmospheric density as a function of latitude, season, and local solar time.[5]

See also

References

  1. ^ a b "Launch Log". Jonathan's Space Report. 21 July 2021. Retrieved 19 November 2021.
  2. ^ a b "Display: DADE-A". NASA. 28 October 2021. Retrieved 19 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ "Display: DADE-B". NASA. 28 October 2021. Retrieved 19 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  4. ^ "Experiment: Atmospheric Composition Mass Spectrometer". NASA. 28 October 2021. Retrieved 19 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  5. ^ "Experiment: Atmospheric Drag Density". NASA. 28 October 2021. Retrieved 19 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.