Category:Interim Cryogenic Propulsion Stage

**Interim Cryogenic Propulsion Stage‎**
	rocket stage in NASA's Space Launch System
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Instance of	rocket model;
Subclass of	rocket stage (Space Launch System Block 1, 3);
Country of origin	United States of America;
Based on	Delta Cryogenic Second Stage;
Manufacturer	Boeing Defense, Space & Security; United Launch Alliance;
Powered by	RL-10B-2 (1, ICPS-1); RL-10C-2 (1, ICPS-2, ICPS-3);
Mass	32,748 kg (launch weight); 3,700 kg (dry weight);
Diameter	5.1 m;
Height	13.7 m;
Authority file
	Q109680477;
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Subcategories

This category has the following 4 subcategories, out of 4 total.

The following 6 files are in this category, out of 6 total.