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BCP-2000
NPP Credit: Manufacturer Image |
American Ball satellite bus in the 1000-kg class to accommodate high-precision optical surveillance payloads.
AKA: NPP;SBSS. Status: Operational 1999. First Launch: 1999-06-20. Last Launch: 2011-10-28. Number: 7 .
More at: BCP-2000.
Subtopics
| QuikScat American earth sea satellite. One launch, 1999.06.20. Built under a NASA rapid delivery contract. Carried the SeaWinds scatterometer for remote sensing of ocean winds. Earth observing satellite built by Ball Aerospace for NASA, USA. Launched 1999. Used the BCP-2000 bus. |
| QuickBird American civilian surveillance satellite. One launch, 2001.10.18. The QuickBird commercial imaging satellite was owned by DigitalGlobe (formerly EarthWatch) and used a Ball BCP2000 bus with a launch mass of 1028 kg and a dry mass of about 995 kg. Earth observing satellite built by Ball Aerospace for Earthwatch Inc. => DigitalGlobe, USA. Launched 2000 - 2001. Used the BCP-2000 bus. |
| ICESat American earth land resources satellite. One launch, 2003.01.13. Laser Altimetry Mission satellite built by Ball Aerospace for NASA, USA. Launched 2003. Used the BCP-2000 bus. |
| Cloudsat American earth weather satellite. One launch, 2006.04.28. Earth Observation satellite built by Ball Aerospace for NASA, USAF STP (Space Test Program), USA. Launched 2006. Used the BCP-2000 bus. |
| SBSS 1 Space Surveillance satellite built by Northrop Grumman Space Technology (prime); Boeing; Ball Aerospace (bus) for Missile Defense Agency (MDA) through the U.S. Air Force Space & Missile Systems Center (SMC),, USA. Launched 2010. Used the BCP-2000. Launched 2010. |
| GFO 2 Altimetry satellite built by Ball Aerospace for US Navy. Used the BCP-2000 bus. |
Family:
Earth,
MX,
Surveillance.
Country:
USA.
Launch Vehicles:
Titan,
Thor,
R-14,
Kosmos 11K65M,
Titan II SLV,
Delta 7920-10C,
Delta 7420-10C,
Delta 7320-10,
Minotaur IV.
Launch Sites:
Vandenberg SLC2W,
Vandenberg SLC4W,
Plesetsk LC132/1.
Bibliography:
12147,
12148.
Photo Gallery
| ICESat Credit: Manufacturer Image |
| QuickBird 1 Credit: Manufacturer Image |
| USA 216 Credit: Manufacturer Image |
| Cloudsat Credit: Manufacturer Image |
1999 June 20 - .
02:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan II SLV.
- QuikScat - .
Nation: USA.
Agency: NASA Greenbelt.
Manufacturer: Ball.
Class: Earth.
Type: Sea satellite. Spacecraft: BCP-2000.
USAF Sat Cat: 25789 . COSPAR: 1999-034A. Apogee: 802 km (498 mi). Perigee: 802 km (498 mi). Inclination: 98.60 deg. Period: 100.90 min.
NASA's QuikScat carried the SeaWinds scatterometer for remote sensing of ocean winds. The Titan 2's second stage shut down at 02:20 GMT and then coasted to apogee still attached to the QuikScat. The Titan second stage vernier thrusters ignited at apogee to raise perigee, leaving QuikScat in a 280 km x 813 km x 98.7 degree parking orbit. The QuikScat's own hydrazine propulsion system then fired to raise the perigee over a period of weeks.
2000 November 20 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Second stage failed to restart at apogee..
Failed Stage: 2.
- QuickBird 1 - .
Mass: 950 kg (2,090 lb). Nation: USA.
Agency: DigitalGlobe.
Manufacturer: Ball.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: BCP-2000.
Decay Date: 2000-11-21 . USAF Sat Cat: 26617 . COSPAR: 2000-074A. Apogee: 614 km (381 mi). Perigee: 80 km (49 mi). Inclination: 65.70 deg. Period: 91.49 min.
The Kosmos-3M second stage entered an 81 x 614 km x 65.8 deg orbit but failed to restart at apogee, and reentered at the next perigee over Uruguay. The loss of the QuickBird 1 satellite was a heavy blow to EarthWatch Inc. QuickBird1 was a 1-m resolution commerical imaging satellite using a Ball Aerospace BCP-2000 bus. Their earlier satellite, EarlyBird, failed after a few days in orbit in December 1997. EarthWatch's rival, SpaceImaging, lost one satellite as well but its second Ikonos was operating in orbit.
2001 October 18 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10.
- QuickBird 2 - .
Mass: 980 kg (2,160 lb). Nation: USA.
Agency: DigitalGlobe.
Manufacturer: Ball.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: BCP-2000.
Decay Date: 2015-01-27 . USAF Sat Cat: 26953 . COSPAR: 2001-047A. Apogee: 471 km (292 mi). Perigee: 471 km (292 mi). Inclination: 97.20 deg. Period: 94.00 min.
The QuickBird commercial imaging satellite was owned by DigitalGlobe (formerly EarthWatch) and used a Ball BCP2000 bus with a launch mass of 1028 kg and a dry mass of about 995 kg. The Delta upper stage entered a 185 x 472 km x 98.1 deg orbit at 1902 GMT. At 1948 GMT it reached apogee and fired again to deploy QuickBird into a 461 x 465 km x 97.2 deg orbit. The Delta then made a series of unusual depletion burns, lowering its perigee to 167 km and changing inclination to 108.9 deg.
Quickbird 2 was to be operational after a few months of calibration and "ground-truth" checkouts to market high resolution images. The 1.0 tonne satellite was reported to be capable of images with a resolution as small as 0.6 meter, though the standard products were to be coarser. Unlike the comparable quality images from IKONOS images, some of which are currently marketed exclusively to the US military, all Quickbird 2 images may be available in the open market.
2003 January 13 - .
00:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10.
- ICESat - .
Payload: EOS-LAM. Mass: 1,000 kg (2,200 lb). Nation: USA.
Agency: NASA.
Manufacturer: Ball.
Class: Earth.
Type: Sea satellite. Spacecraft: BCP-2000.
Decay Date: 2010-08-30 . USAF Sat Cat: 27642 . COSPAR: 2003-002A. Apogee: 610 km (379 mi). Perigee: 593 km (368 mi). Inclination: 94.01 deg. Period: 96.56 min. Oceanography, gravimetry, altimetry mission. Delayed from March 30, May 12, August 30, September 10, December 15 and 20, 2002; and Jan. 11 and 12, 2003..
2006 April 28 - .
10:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- Cloudsat - .
Mass: 848 kg (1,869 lb). Nation: USA.
Agency: CSA,
NASA,
USAF.
Manufacturer: Ball.
Class: Earth.
Type: Weather satellite. Spacecraft: BCP-2000.
USAF Sat Cat: 29107 . COSPAR: 2006-016A. Apogee: 704 km (437 mi). Perigee: 702 km (436 mi). Inclination: 98.20 deg. Period: 98.80 min. Cloudsat carried a 94 GHz cloud profiling radar. Both the Cloudsat and Calipso satellites were in the A-train polar constellation, in the same orbit as the large Aqua and Aura satellites..
2010 September 30 - .
Launch Site:
Vandenberg.
LV Family:
Peacekeeper.
Launch Vehicle:
Minotaur IV.
- USA 216 - .
Payload: SBSS. Mass: 1,031 kg (2,272 lb). Nation: USA.
Agency: USAF.
Manufacturer: Ball.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: BCP-2000.
USAF Sat Cat: 37168 . COSPAR: 2010-048A. Apogee: 633 km (393 mi). Perigee: 632 km (392 mi). Inclination: 98.00 deg. Period: 97.40 min. First Space-Based Surveillance Satellite; designed to track satellites and orbital junk from a space-based vantage point..
2011 October 28 - .
09:48 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7920-10C.
- NPP - .
Mass: 1,976 kg (4,356 lb). Nation: USA.
Class: Earth.
Type: Weather satellite. Spacecraft: BCP-2000.
USAF Sat Cat: 37849 . COSPAR: 2011-061A. Apogee: 823 km (511 mi). Perigee: 818 km (508 mi). Inclination: 98.70 deg. Period: 101.30 min.
NPP Preparatory Project weather satellite, using payloads from the cancelled National Polar Orbiting Environmental Satellite System. The NPP provided a stopgap between the last of the Advanced TIROS-N polar weather satellites and the first Joint Polar Satellite System satellite to be launched in a few years.
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