AJ-60A
![]() An AJ-60A booster, without nosecone attached, being fitted to an Atlas V | |
Manufacturer | Aerojet Rocketdyne |
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Country of origin | USA |
Used on | Atlas V |
General characteristics | |
Height | 17.0 m (669 in) |
Diameter | 1.6 m (62 in) |
Gross mass | 46,697 kg (102,949 lb) |
Engine details | |
Maximum thrust | 1,688.4 kN (379,600 lbf) |
Burn time | 94 seconds |
Propellant | HTPB/AP (APCP) |
AJ-60A is a solid rocket booster produced by Aerojet Rocketdyne. Up to 2020 they were used as strap-on boosters on all United Launch Alliance Atlas V rocket configurations. They continue to be used on the Atlas V N22 configuration used to launch the Boeing Starliner.[1]
History
The AJ-60A rocket motor was developed between 1999 and 2003 for use on the Atlas V.[2]
On January 19, 2006 the New Horizons spacecraft to Pluto was launched directly into a solar-escape trajectory at 16.26 kilometers per second (58,536 km/h; 36,373 mph) from Cape Canaveral using an Atlas V version with 5 of these SRBs and Star 48B third stage.[3] New Horizons passed the Moon's orbit in just nine hours.[4][5]
In 2015, ULA announced that the Atlas V will switch to new GEM 63 boosters produced by Northrop Grumman Innovation Systems. (GEM 63XL, a stretched version of the GEM 63 booster will be used on the upcoming Vulcan rocket.)[6] The first Atlas V launched with GEM 63 boosters on November 13, 2020.[7]
Design
AJ-60A is a solid fueled rocket burning HTPB-based composite solid propellant.[8] The casing is composed of a graphite-epoxy composite, and the engine throat and nozzle are made of carbon-phenolic composite. As configured for use on Atlas V, the nozzle is fixed at a 3 degree cant away from the attachment point, but Aerojet offers a variant with thrust vectoring capability.[2] The Atlas V configuration also features an inward slanting nosecone, but it is available with a conventional nosecone or none at all for use on other rockets. The stages are designed to be transported by truck.[8]
References
- ^ Clark, Stephen (May 15, 2021). "Billion-dollar missile defense satellite ready for launch Monday in Florida". Spaceflight Now. Retrieved August 8, 2024.
- ^ a b "Atlas V Solid Rocket Booster". Archived from the original on March 14, 2017. Retrieved January 6, 2016.
- ^ Scharf, Caleb A. (February 25, 2013). "The Fastest Spacecraft Ever?". Scientific American. Retrieved July 12, 2017.
- ^ Neufeld, Michael (July 10, 2015). "First Mission to Pluto: The Difficult Birth of New Horizons". Smithsonian. Retrieved April 21, 2018.
- ^ "New Horizons: Mission Overview" (PDF). International Launch Services. January 2006. Archived from the original (PDF) on September 9, 2016. Retrieved April 21, 2018.
- ^ Jason Rhian (23 September 2015). "ULA selects Orbital ATK's GEM 63/63 XL SRBs for Atlas V and Vulcan boosters". Spaceflight Insider. Archived from the original on 11 January 2016. Retrieved 6 January 2016.
- ^ Northrop Grumman Ships GEM 63 Engines to United Launch Alliance For Atlas V July 2020
- ^ a b "Atlas V User's Guide 2010" (PDF). 2010. Archived from the original (PDF) on March 6, 2012. Retrieved January 6, 2016.
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fuel
Cryogenic |
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Semi- cryogenic |
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Storable |
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Other |
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![](http://upload.wikimedia.org/wikipedia/commons/thumb/4/4d/RS-68_rocket_engine_test.jpg/120px-RS-68_rocket_engine_test.jpg)
fuel
- China
- Europe
- India
- Iran
- Salman
- Rafe
- Israel
- Japan
- USA
- * Different versions of the engine use different propellant combinations
- Engines in italics are under development