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DSP
Defense Support Program
Part of the DSP (Defence Support Program) program
DSP is the 2nd generation DSP satellite.
Spacecraft
Spacecraft spin slowly (6 rpm) about the nadir axis to permit scanning of the Earth by the detector system. Zero momentum stabilized using a reaction wheel to counter the spacecraft spin. Body mounted cells and deploablye panels generate roughly 680 W.
Payload
Payload includes 3.6 m Schmidt telescope with 2000 element IR sensor, nuclear detection sensors.
Country of Origin | United States |
Customer/User | USAF |
Manufacturer(s) | TRW |
Size | 2.8 m dia. by 2.9 m tall cylinder |
Orbit | Geosynchronous |
Design Life | 3 years (5 year goal) |
Launch Facts
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Name | Int'l Desig. | Date | Site | Vehicle | Orbit | Mass(kg) |
Notes |
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DSP F6 | 1976-059A | 6/26/76 | ESMC | Titan 3C | GEO | 820 |
Defense Support Program |
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DSP F7 | 1977-007A | 2/6/77 | ESMC | Titan 3C | GEO | 820 |
Defense Support Program |
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DSP F8 | 1979-053A | 6/10/79 | ESMC | Titan 3C | GEO | 820 |
Defense Support Program |
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DSP F9 | 1981-025A | 3/16/81 | ESMC | Titan 3C | GEO | |
Defense Support Program |
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DSP F10 | 1982-019A | 3/6/82 | ESMC | Titan 3C | GEO | |
Defense Support Program |
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DSP F11 | 1984-037A | 4/15/84 | ESMC | Titan 34D | GEO | |
Defense Support Program |
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DSP F12 (USA 7) | 1984-129A | 12/22/84 | ESMC | Titan 34D | GEO | |
Defense Support Program |
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DSP F13 (USA 28) | 1987-097A | 11/29/87 | ESMC | Titan 34D | GEO | |
Defense Support Program |
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Information in The Mission and Spacecraft Library is provided without
warranty or guarantee. USE AT YOUR OWN RISK.
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