USA-214

Satellite description

The USA-214 satellite was constructed by Lockheed Martin Space, and is based on the A2100 satellite bus. The satellite has a mass of 6168 kg and a design life of 14 years. It will be used to provide super high frequency (SHF) and extremely high frequency (EHF) communications for the United States Armed Forces, as well as those of the United Kingdom, the Netherlands, and Canada.

Launch

Though initially scheduled for launch on 30 July 2010, delays with the launch vehicle pushed flight back to 10 August 2010, and finally to 14 August 2010.

USA-214 was launched by United Launch Alliance, aboard an Atlas V 531 flying from Space Launch Complex-41 (SLC-41) at the Cape Canaveral Air Force Station (CCAFS). The launch occurred at 11:07:00 UTC on 14 August 2010, and resulted in the satellite being deployed successfully into a geostationary transfer orbit (GTO) with a perigee of 221 km, an apogee of 50179 km, and 22.2° Orbital inclination.

Anomaly

The satellite was intended to maneuver from the transfer orbit into which it was launched to its operational geosynchronous orbit by means of a liquid apogee engine (LAE) and several Hall-effect thrusters, a process which normally takes 105 days. However, the satellite's Liquid Apogee Engine malfunctioned shortly after ignition on both its first burn on 15 August 2010 and a second attempt on 17 August 2010, and it was declared inoperable.

To solve the problem, the perigee altitude was raised to 4700 km using twelve firings of the smaller Reaction Engine Assembly thrusters, originally intended for attitude control during LAE maneuvers. From this altitude, the solar arrays were deployed and the orbit was raised toward the operational orbit over the course of nine months using the 0.27 Newton Hall effect thruster, a form of electric propulsion which is highly efficient, but produces very low thrust and is therefore very slow.

The problem with the liquid apogee engine was later blamed on a piece of cloth accidentally left in a fuel line leading up to the engine while the line was taken apart for repair during the manufacture of the satellite. The cloth was likely placed in the line to prevent impurities from entering the fuel line and did not get removed when the line was put back together.

References

References

1. "AEHF 1 (USA 214)". Heavens Above.
2. "Atlas V AEHF-1 Mission Overview". United Launch Alliance.
3. (4 November 2020). "AEHF 1, 2, 3, 4, 5, 6". Gunter's Space Page.
4. (2010-07-15). "AEHF-1 Launch Delayed". Air Force Magazine.
5. Ray, Justin. (14 August 2010). "Rise and shine: Atlas 5 rocket successfully soars at dawn". Spaceflight Now.
6. McDowell, Jonathan. (12 August 2010). "Issue 632". Jonathan's Space Report.
7. Ray, Justin. (30 August 2010). "Military satellite relying on backup plan to save itself". Spaceflight Now.
8. Butler, Amy. (15 November 2010). "Japanese Engine Not AEHF Issue: USAF Official". Aviation Week.
9. Butler, Amy. (22 November 2010). "USAF: AEHF-1 Engine Failure An Anomaly". Aviation Week.
10. Ray, Justin (2 September 2010), ''Spaceflight Now'', [http://spaceflightnow.com/atlas/av019/100902inquiry.html Investigators probing what went wrong with AEHF 1] (accessed 14 December 2011)
11. "Main engine probably not to blame for AEHF-1 trouble".
12. Ray, Justin (9 October 2011), ''Spaceflight Now'', [http://spaceflightnow.com/atlas/av019/111009.html Air Force satellite's epic ascent should finish soon] (accessed 14 December 2011)
13. (17 March 2012). "Delicate rescue saves stranded US$1.7 billion U.S. satellite".