Atlas H
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This rocket article contains payload capacity, but does not include orbital altitude or inclination, which greatly affects the capacity. |
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Page Module:Infobox/styles.css has no content.| Lua error in package.lua at line 80: module 'Module:InfoboxImage/data' not found. Launch of the last Atlas H with NOSS-9. | |
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| Project cost | Script error: No such module "WikidataIB". |
| Cost per launch | Script error: No such module "WikidataIB". |
| Cost per year | Script error: No such module "WikidataIB". |
| Size | |
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| Stages | Script error: No such module "WikidataIB". |
| Associated rockets | |
| Family | Script error: No such module "WikidataIB". |
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| Launch history | |
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| Total launches | Script error: No such module "WikidataIB". |
| Success(es) | Script error: No such module "WikidataIB". |
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| Landings | Script error: No such module "WikidataIB". |
| First flight | Script error: No such module "WikidataIB". |
| Last flight | Script error: No such module "WikidataIB". |
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| Boosters | |
| No. boosters | 1 |
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| Propellant mass | Script error: No such module "WikidataIB". |
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| Total thrust | 1,901.6 kN (427,500 lbf) |
| Specific impulse | Script error: No such module "WikidataIB". |
| Burn time | Script error: No such module "WikidataIB". |
| Propellant | Script error: No such module "WikidataIB". |
| First stage | |
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The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile.[1] It was a member of the Atlas family of rockets, and was used to launch five clusters of NOSS satellites for the US National Reconnaissance Office.[1] Two flights also carried LiPS satellites, as secondary payloads for the United States Naval Research Laboratory.[1]
The Atlas H was a stage and a half rocket, using the enhanced Atlas rocket designed for use as the first stage of the Atlas G rocket,[2] which differed from the Atlas H in having a Centaur upper stage. This stage was later reused as the first stage of the Atlas I. In practice, an MSD upper stage was flown on all five launches.[3]
Atlas H could put a payload of 3,630 kg (8,000 lb) into low Earth orbit, or a payload of 2,255 kg (4,971 lb) into a geostationary transfer orbit.[1]
Launches
The Atlas H was launched five times from Vandenberg SLC3E:[1]
| Date | Mission | Mass (kg) | Apogee (km) | Perigee (km) | Inclination º |
|---|---|---|---|---|---|
| 1983 February 9 | NOSS 4 - PARCAE 5 / OPS 0252 | 700 | 1,186 | 1,063 | 63.40 |
| SSB - SSU | 700 | 1,489 | 733 | 63.40 | |
| SSD (NOSS 4) - NOSS-Subsat 4-4 | 1,419 | 796 | 63.40 | ||
| SSC - SSU | 1,173 | 1,043 | 63.50 | ||
| SSA - SSU | 1,166 | 1,051 | 63.40 | ||
| SSA (NOSS 4) - NOSS-Subsat 4-1 / OPS 0252 DEB | 1,164 | 1,051 | 63.50 | ||
| LIPS 2 | 1,399 | 822 | 63.30 | ||
| 1983 June 9 | NOSS 5 - PARCAE 6 / OPS 6432 | 700 | 1,167 | 1,049 | 63.40 |
| GB1 - SSU | 1,167 | 1,049 | 63.40 | ||
| GB3 - SSU | 1,166 | 1,049 | 63.40 | ||
| GB2 - SSU | 1,167 | 1,049 | 63.40 | ||
| 1984 February 5 | NOSS 6 - PARCAE 7 / OPS 8737 | 700 | 1,172 | 1,052 | 63.40 |
| JD1 - SSU | 1,172 | 1,052 | 63.40 | ||
| JD2 - SSU | 1,172 | 1,052 | 63.40 | ||
| JD3 - SSU | 1,172 | 1,052 | 63.40 | ||
| 1986 February 9 | USA 15 - PARCAE 8 | 700 | 1,166 | 1,049 | 63.00 |
| USA 18 - SSU | 1,407 | 817 | 63.41 | ||
| USA 16 - SSU | 1,161 | 1,055 | 63.00 | ||
| USA 17 - SSU | 1,165 | 1,055 | 63.00 | ||
| 1987 May 15 | USA 22 - PARCAE 9 | 700 | 1,179 | 1,045 | 62.90 |
| LIPS 3 | 1,316 | 899 | 63.40 | ||
| USA 25 - SSU | 1,178 | 1,035 | 62.60 | ||
| USA 24 - SSU | 1,184 | 1,046 | 63.20 | ||
| USA 23 - SSU | 1,170 | 1,039 | 63.40 |
References
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- ^ a b c d e Page Module:Citation/CS1/styles.css has no content."Atlas H". www.astronautix.com. Retrieved 2023-10-09.
- ^ Encyclopedia Astronautica - Atlas
- ^ Gunter's Space Page - Atlas-H MSD
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