Category:AJ60A (rocket engine)

**AJ-60A**
	solid rocket booster by Aerojet Rocketdyne
	Upload media
	Wikipedia
Instance of	engine model;
Subclass of	solid rocket booster;
Country of origin	United States of America;
Manufacturer	Aerojet Rocketdyne;
First flight	17 July 2003;
Significant event	development (1999–2003); maiden flight (Atlas V 521, 2003); service retirement (2020);
Source of energy	solid rocket propellant (hydroxyl-terminated polybutadiene);
Mass	46,697 kg;
Diameter	1.5748 m;
Height	16.9926 m;
Authority file
	Q22001987;
	Reasonator; Scholia; Wikidocumentaries; PetScan; statistics; WikiMap; Locator tool; KML file; Search depicted;

English: The AJ-60A is a solid-propellant booster rocket used on Atlas V launch vehicles between 2003 and 2020.

Media in category "AJ60A (rocket engine)"

The following 12 files are in this category, out of 12 total.