Antares A-ONE

Antares A-ONE mission was the maiden flight of Orbital Sciences Corporation' Antares launch vehicle including the ascent to space and accurate delivery of a simulated payload, the Cygnus Mass Simulator (CMS), which was launched 21 April 2013.[5] It was launched from Pad 0A at the Mid-Atlantic Regional Spaceport (MARS), Wallops Flight Facility, Virginia.[5] The simulated payload simulates the mass of the Cygnus cargo spacecraft.[5] This dummy payload was sent into an orbit of 240 km × 260 km (150 mi × 160 mi) with an orbital inclination of 51.6°, the same launch profile it uses for Orbital's Cygnus cargo supply missions to the International Space Station (ISS) for NASA.[5]

Antares A-ONE
The Antares 110 lifts off at the start of the mission
NamesSimulated Cygnus Payload [1]
Mission typeTest flight
OperatorOrbital Sciences Corporation
COSPAR ID2013-016D
SATCAT no.39145
Websitehttps://news.northropgrumman.com/
Mission duration19 days
Spacecraft properties
SpacecraftCygnus mass simulator
ManufacturerOrbital Sciences Corporation
Launch mass3,800 kg (8,400 lb)
Dimensions5.061 m × 2.896 m (16.60 ft × 9.50 ft)
Start of mission
Launch date21 April 2013, 21:00:00 UTC[2][3]
RocketAntares 110[4]
Launch siteWallops Pad 0A
ContractorOrbital Sciences Corporation
End of mission
DisposalDeorbited
Decay date10 May 2013
Orbital parameters
Reference systemGeocentric orbit[5]
RegimeLow Earth orbit
Perigee altitude240 km (150 mi)
Apogee altitude260 km (160 mi)
Inclination51.6°

Orbital Sciences insignia 

This launch along with several other activities leading up to it, are paid milestones under NASA's Commercial Orbital Transportation Services (COTS) program.[6]

Primary payload

The primary payload was the Cygnus Mass Simulator. It had a height of 5.061 m (16.60 ft), a diameter of 2.896 m (9 ft 6.0 in) and a mass of 3,800 kg (8,400 lb).[7] It was equipped with 22 accelerometers, 2 microphones, 12 digital thermometers, 24 thermocouples and 12 strain gages.[7]

Secondary payloads

Four Spaceflight Industries Inc. CubeSat nanosatellites were deployed from the dummy payload.[8]

The secondary payloads were four CubeSats that were deployed from the CMS.[7] Three of them were PhoneSats, 1U CubeSats built by NASA's Ames Research Center.[7] These were named Alexander, Graham and Bell, after the Alexander Graham Bell, inventor of the telephone.[7] The purpose of these three satellites was to demonstrate the use of smartphones as avionics in CubeSats.[7] They each had a mass of 1,124 kg (2,478 lb) and were powered by lithium batteries.[7] The fourth nanosat was a 3U CubeSat, called Dove-1, built by Cosmogia Inc. It carried a "technology development Earth imagery experiment" using the Earth's magnetic field for attitude control.[7][9]

Mission timeline

  • Lift off of the Antares launch vehicle occurs two seconds after the first stage engines are ignited
  • The first stage engines shut off 228 seconds after lift-off
  • At 233 seconds, the first stage separates from the second
  • At 317 seconds, the payload fairing is jettisoned
  • At 326 seconds, the second stage's engine is ignited
  • At 481 seconds, the second stage is shut off
  • At 601 seconds, the Cygnus Mass Simulator separates [5]
AttemptPlannedResultTurnaroundReasonDecision pointWeather go (%)Notes
117 Apr 2013, 5:00:00 pmscrubbedtechnical17 Apr 2013, 4:44 pm ​(T-12:00 hold)60% [10]Premature disconnect of upper stage umbilical cable during T-12:00 hold [11]
220 Apr 2013, 6:10:00 pmscrubbed3 days, 1 hour, 10 minutesweather20 Apr 2013, 4:30 pm90%[12]
321 Apr 2013, 5:00:00 pmsuccess0 days, 22 hours, 50 minutes80%First flight of Antares [13]

Gallery

See also

References

External links