Angara (rocket family)
Cancelled or proposed

Angara (rocket family)

Section Title: Cancelled or proposed
Table Section Text: None

Version	Angara 1.1 (Cancelled)	Angara A3 (Proposed)	Angara A5P (Proposed)	Angara A5V (Proposed)	Angara A7 (Proposed)	Angara A7.2B (Proposed)

Boosters	N/A	2xURM-1	4xURM-1	4xURM-1	6xURM-1	6xURM-1

First stage	1xURM-1	1xURM-1	1xURM-1	1xURM-1	1xURM-1	1xURM-1

Second stage	Briz-KM	Modified Block I	–	URM-2V	KVTK-A7	URM-2

Third stage (not used for LEO)	–	Briz-M/RCAF	Blok DM-03/KVTK	KVTK2-А7В

Thrust (at sea level)	1.92 MN	5.77 MN	9.61 MN	10.57 MN	13.44 MN

Launch weight	149 t	481 t	713 t	815 - 821 t	1133 t	1323 t

Height (maximal)	34.9 m	45.8 m	?	?	?	65,7 m

Payload (LEO 200 km)	2.0 t	14.6 t	18.0 t	35 - 40 t	35 t	50 t

Payload (GTO)	–	2.4/3.6 t	–	11.9 - 13.3 t	12.5 t	19 t

Payload (GEO)	–	1.0/2.0 t	–	7.2 - 8 t	7.6 t	11.4 t

Sentence(s)

The proposed Angara A7 weighs 1133 tonnes and capable of putting 35 tonnes into a 200 km orbit or delivering 12.5 tonnes to GTO with KVTK-A7 as the second stage in place of the URM-2.

final_sentence: The proposed Angara A7 weighs 1133 tonnes and capable of putting 35 tonnes into a 200 km orbit or delivering 12.5 tonnes to GTO with KVTK-A7 as the second stage in place of the URM-2.