TDRS-9

Summary

TDRS-9
TDRS-I.jpg
TDRS-I undergoing processing before launch
Mission typeCommunication
OperatorNASA
COSPAR ID2002-011A
SATCAT no.27389Edit this on Wikidata
Mission durationPlanned: 11 years
Elapsed: 19 years, 2 months, 7 days
Spacecraft properties
BusBSS-601
ManufacturerBoeing SDC
Launch mass3,180 kilograms (7,010 lb)[1]
Start of mission
Launch date8 March 2002, 22:59 (2002-03-08UTC22:59) UTC
RocketAtlas IIA
Launch siteCape Canaveral SLC-36A
ContractorILS
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude151° West
173.5° West
64.5° West
Perigee altitude35,768 kilometers (22,225 mi)
Apogee altitude35,809 kilometers (22,251 mi)
Inclination0 degrees
Epoch8 March 2002, 17:59:00 UTC[2]
TDRS I Logo.png  

TDRS-9, known before launch as TDRS-I, is an American communications satellite which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by the Boeing Satellite Development Center, formerly Hughes Space and Communications, and is based on the BSS-601 satellite bus.[3] It was the second Advanced TDRS, or second-generation Tracking and Data Relay Satellite, to be launched.

History

The launch of TDRS-I

An Atlas IIA rocket was used to launch TDRS-I, under a contract with International Launch Services. The launch occurred at 22:59 GMT on 8 March 2002, and used Space Launch Complex 36A at the Cape Canaveral Air Force Station.[4]

Deployment and problems

TDRS-9 separated from its carrier rocket into a geosynchronous transfer orbit. At 06:00 on 6 October, following a series of apogee burns, it reached geostationary orbit.[5] The orbit raising maneuvers were originally scheduled to take ten days, but ended up lasting six months due to a problem with the system used to pressurize its number two fuel tank.[6] A valve used to release helium into the tank failed to open. This was later established to have been due to a wiring error prior to launch. Engineers developed a solution which involved pressurizing the tank using the pressurization system from the number one tank, which was still working, once the propellant in that tank had been used.[6] When orbit raising operations resumed on 19 March, it was estimated that it would take two months to raise the satellite's orbit. It was later discovered that only using fuel from the number one tank upset the satellite's center of mass, causing the satellite to tumble when its main engines were fired. Controllers were able to compensate for this, however it took longer to raise the orbit as a result.[6]

Operations

Upon reaching geostationary orbit, TDRS-I was initially placed at a longitude 151 degrees west of the Greenwich Meridian, and following on-orbit testing it received its operational designation, TDRS-9. In October 2003 it was moved from 151° West, and it arrived at 173.5° West in January 2004. It remained there until September, when it was moved to 64.5° West, arriving in March 2005.[7] Engineers believe that the problems with its fuel tank pressurization system will not affect its operational lifespan.

Location of TDRS as of 22 May 2020
Location of TDRS as of March 2019

References

  1. ^ "UCS Satellite Database". Union of Concerned Scientists. 1 July 2009. Retrieved 10 August 2009. CS1 maint: discouraged parameter (link)
  2. ^ "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. Retrieved 2 May 2018.
  3. ^ Krebs, Gunter. "TDRS 8, 9, 10". Gunter's Space Page. Retrieved 10 August 2009. CS1 maint: discouraged parameter (link)
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 10 August 2009. CS1 maint: discouraged parameter (link)
  5. ^ McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Retrieved 10 August 2009. CS1 maint: discouraged parameter (link)
  6. ^ a b c Harland, David M; Lorenz, Ralph D. (2005). Space Systems Failures (2006 ed.). Chichester: Springer-Praxis. ISBN 0-387-21519-0.
  7. ^ "TDRS 9". TSE. Retrieved 10 August 2009. CS1 maint: discouraged parameter (link)