Angara A5
FunctionHeavy-lift launch vehicle
ManufacturerKhrunichevKBKhA
Country-originRussia
CplUS$100 million (2021) [1]
Height55.4 m (182 ft)
Width8.86 m (29.1 ft)
Mass171,500–790,000 kg (378,100–1,741,700 lb)
Stages2-3
FamilyAngara
ComparableNaro-1
StatusActive
SitesPlesetsk, Site 35
Vostochny, Site 1A
Launches5
Success4
Partial1
First23 December 2014
Last19 June 2025 (most recent)
Angara A5
LocationLEO (Plesetsk)
Mass24,500 kg (54,000 lb)
Angara A5
LocationGTO (Plesetsk)
Mass5,400 kg (11,900 lb) - 7,500 kg (16,500 lb)
URM-1
booster
Number4
Engines1 × RD-191
Thrust1,920 kN (430,000 lbf)
Total7,680 kN (1,730,000 lbf)
Si310.7 isp
Burntime214 seconds
FuelLOX / RP-1
URM-1
stage
StagenoFirst
Engines1 × RD-191
Thrust1,920 kN (430,000 lbf)
Si310.7 isp
Burntime325 seconds
FuelLOX / RP-1
URM-2
stage
StagenoSecond
Engines1 × RD-0124A
Thrust294.3 kN (66,200 lbf)
Si359 isp
Burntime424 seconds
FuelLOX / RP-1
Briz-M (optional)
stage
StagenoThird
Engines1 × S5.98M
Thrust19.6 kN (4,400 lbf)
Si326 isp
Burntime3,000 seconds
FuelN2O4 / UDMH
Blok DM-03 (optional)
stage
StagenoThird
Engines1 × RD-58MF
Thrust19.6 kN (4,400 lbf)
Si326 isp
Burntime3,000 seconds
FuelLOX / RP-1
KVTK (optional, under development)
stage
StagenoThird
Engines1 × RD-0146D
Thrust68.6 kN (15,400 lbf)
Si463 isp
Burntime1,350 seconds
FuelLOX / LH2

Angara A5 (Russian: Ангара-А5), is a Russian expendable heavy lift launch vehicle which consists of one URM-1 core and four URM-1 boosters, a 3.6-metre (12-foot) URM-2 second stage, and an upper stage, either the Briz-M, Blok DM-03 or the KVTK.[2] Weighing 773 tonnes (1,704,000 lb) at lift-off, Angara A5 has a payload capacity of 24.5 tonnes (54,000 lb) to a 200 km (120 mi) x 60° orbit. Angara A5 is able to deliver 5.4 tonnes (12,000 lb) to GTO with Briz-M, or 7.5 tonnes (17,000 lb) to the same orbit with KVTK.[2] Adding a kick stage increases the height of the rocket.

In the Angara A5, the four URM-1s used as boosters operate at full thrust for approximately 214 seconds, then separate. The URM-1 forming the vehicle's core is operated at full thrust for lift off, then throttled down to 30% to conserve propellant. The core is throttled back up after the boosters have separated and continues burning for another 110 seconds.[3]

The first Angara A5 test flight was launched on 23 December 2014. The second test flight was launched on 14 December 2020 from Plesetsk.[4]

Some official models show the Angara carrying an Orel crew capsule spacecraft with an abort tower.

Launches

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See also

References

  1. ^ "MGM n°3". 24 December 2021. Retrieved 24 December 2021.
  2. ^ "ГКНПЦ имени М.В.Хруничева | Семейство ракет-носителей "Ангара"". 2017-01-18. Archived 2017-01-18 at the Wayback Machine. Retrieved 2023-11-26.
  3. ^ "Angara A5 - Spaceflight101". 2015-09-25. Archived 2015-09-25 at the Wayback Machine. Retrieved 2023-11-26.
  4. ^ "Launch Schedule – Spaceflight Now". Retrieved 2023-11-26.