Archimedes (rocket engine)

Liquid fuel rocket engine

ArchimedesCountry of origin| United States
New Zealand

|

Designer| Rocket Lab
Manufacturer| Rocket Lab
Application| First- and second-stage engine
Status| In development
Liquid-fuel engine
Propellant| LOX / CH4
Cycle| Oxidizer-rich staged combustion
Configuration
Chamber| 1
Performance
Thrust, vacuum| 890 kN (200,000 lbf)
Thrust, sea-level| 730 kN (165,000 lbf)
Throttle range| 50–100%
Specific impulse, vacuum| 365 s (3.58 km/s)
Specific impulse, sea-level| 329 s (3.23 km/s)
Used in
Neutron
References
References| [1][2]

Archimedes is a liquid-fuel rocket engine burning liquid oxygen and liquid methane in an oxidizer-rich staged combustion cycle.[1][2] It is designed by aerospace company Rocket Lab for its Neutron rocket.[3][1]

## History

[edit]

Archimedes was presented on December 2, 2021, in a webcast by Rocket Lab CEO Peter Beck[4] as a fully reusable, gas generator engine using liquid oxygen (LOX) and methane as propellant, a departure from the company's previous Rutherford, which is electrically pump fed. He then stated that it had a thrust of 1 MN (220,000 lbf) and 320 seconds of specific impulse. The same day, the Neutron page on Rocket Lab's website was updated specifying the thrust of the nine Archimedes engines used on the first stage as 5,960 kN (1,340,000 lbf) at sea level and a maximum thrust of 7,530 kN (1,690,000 lbf) and the upper stage's single vacuum optimized Archimedes at 1,110 kN (250,000 lbf). It was expected to have its first hot-fire test during May 2024.[5] In an interview published on the CNBC website, Beck stated that Archimedes would be manufactured in New Zealand and its very simple design had "all the things you want when you have to build an engine that can be reused over and over again."[6]

In the September 21st, 2022 Investor Day Presentation, the engine design had changed to an oxidizer-rich staged combustion cycle.[1] The presentation stated that the sea level version would have a maximum thrust of 730 kN (160,000 lbf) with a specific impulse of 329 seconds and would be able to throttle to 50% of maximum thrust.[citation needed]

Meanwhile, the vacuum optimized version would have a maximum thrust of 890 kN (200,000 lbf), a specific impulse of 367 s and the same throttling capabilities of 50% of maximum thrust.[1][2] It was also implied, but not confirmed, that the engine would be built in the Virginia, USA factory. It was disclosed they would use the Stennis Space Center A-3 Test stand for development testing. They expected to start preburner testing in that or the following quarter, hopefully starting full engine testing at Stennis before the end of 2023, and hoped to be able to launch by mid 2025.[citation needed]

## Design

[edit]

Archimedes is presented as a highly reusable liquid-propellant engine using methane and liquid oxygen in an oxidizer-rich staged combustion cycle.[1][2] There are both sea-level and vacuum variants. The engine is mostly 3D printed,[7] with some of the biggest 3D printers in the world. The rationale for the cycle change from the original gas generator was that they could not get the performance they needed through all the throttle points that a reusable rocket needs, without pushing the turbine temperature and other factors beyond their preset limits. By changing to the higher performing cycle but with lower performance requirements, they were able to lower temperatures and other stress factors and increase margins everywhere, making reusability more attainable.[2]

## See also

[edit]

* Spaceflight portal

* Rocket Lab Neutron
* Rutherford (rocket engine)
* Curie (rocket engine)
* Merlin (rocket engine family)
* SpaceX Raptor

## References

[edit]

1. ^ a b c d e f "2022 Inverstor Day and Neutron Update" (PDF). Rocket Lab. 2022-09-21. Archived from the original (PDF) on 2022-09-22. Retrieved 2022-09-22.
2. ^ a b c d e Rocket Lab 2022 Investor Day & Neutron Update (YouTube video). Rocket Lab. 2022-09-21. Retrieved 2022-09-22.
3. ^ "Neutron Rocket Lab". Rocket Lab. 2021-12-02. Archived from the original on 2021-12-02. Retrieved 2021-12-02.
4. ^ Neutron Rocket - Major Development Update (YouTube video). Rocket Lab. 2021-12-02. Retrieved 2021-12-02.
5. ^ Gebhardt, Chris (2021-12-02). "Neutron switches to methane/oxygen, 1 Meganewton Archimedes engine revealed". NASA SpaceFlight. Archived from the original on 2021-12-02. Retrieved 2021-12-02.
6. ^ Sheetz, Michael (2021-12-02). "Neutron Rocket Lab". CNBC. Archived from the original on 2021-12-02. Retrieved 2021-12-02.
7. ^ "With Senior Advisor to Californian Governor Gavin Newsom, Dee Dee Myers and Rocket Lab 's Peter Beck at Rocket Lab's Long Beach facility. Had a thorough discussion about more opportunities for business between New Zealand and California & how much better we are working together". 12 April 2024.

## External links

[edit]

* Rocket Lab Neutron Rocket

* v
* t
* e

Rocket engines and solid motors for orbital launch vehicles

* Comparison of orbital rocket engines

Liquid
fuel|

| Cryogenic|

| Hydrolox
(LH2 / LOX)|

* China
* YF-73
* YF-75
* YF-75D
* YF-77
* YF-79
* YF-90
* Europe
* HM7B
* Vinci
* Vulcain
* India
* CE-7.5
* CE-20
* Japan
* LE-5
* LE-7
* LE-9
* Russia
* KVD-1 (RD-56)
* RD-0120
* RD-0146
* United States
* BE-3U
* BE-7
* J-2
* RL10
* RS-25
* RS-68

|

Methalox
(CH4 / LOX)|

* China
* BF-20
* Lingyun
* Longyun
* TQ-11
* TQ-12
* TQ-15A
* YF-209
* YF-215
* United States
* BE-4
* Raptor
* Archimedes
* Aeon 1
* Aeon R
* Russia
* RD-0169
* Europe
* Prometheus
* M-10

Semi-
cryogenic|

| Kerolox
(RP-1 / LOX)|

* China
* TH-11
* TH-12
* YF-100
* YF-102
* YF-115
* YF-130
* Welkin
* India
* SCE-200
* Russia
* NK-15
* NK-33, 44
* RD-58
* RD-0105, 0109
* RD-0107, 0108, 0110
* RD-0110R
* RD-0124
* RD-107, 108, 117, 118
* RD-120
* RD-170, 171
* RD-180
* RD-191, 151, 181
* RD-193
* S1.5400
* Spain
* TEPREL
* Ukraine
* RD-8
* RD-801
* RD-810
* United States
* F-1
* H-1
* Kestrel
* LR-79
* LR89
* LR105
* LR70-NA , S-3D
* Merlin
* RS-27
* RS-27A
* RS-56
* S-3D
* Rutherford
* XLR50

|

Storable|

| Hypergolic (Aerozine,
UH 25, MMH, or UDMH
/ N2O4, MON, or HNO3)|

* China
* YF-1, 2, 3
* YF-20, 21, 22, 24, 25
* YF-23
* YF-40
* YF-50D
* Europe
* Aestus
* Astris
* Vexin
* Viking
* India
* PS4
* Vikas
* Israel
* LK-4
* North Korea
* Paektusan LRE along other LREs
* Russia
* 17D61
* RD-0202 to 0206, 0208 to 0213
* RD-0207, 0214
* RD-0216, 0217, 0235
* RD-0233, 0234
* RD-0236
* RD-0237
* RD-0243 to 0245
* RD-0255 to 0257
* RD-215 to 219
* RD-250 to 252, 261, 262
* RD-253, 275
* RD-263, 268, 273
* RD-270
* S5.92
* S5.98M
* Ukraine
* RD-843
* RD-854, 861
* RD-855
* RD-856
* RD-864, 869
* United States
* AJ10
* LR-87
* LR-91
* RS-88*
* TR-201
* XLR81*

|

Other|

* Russia
* RD-109, 119
* RD-211 to 214
* UK
* Gamma
* United States
* Curie
* RS-88*
* XLR81*

Solid
fuel|

* China
* FG-02
* FG-36
* FG-46
* FG-47
* SpaB-65
* SpaB-140C
* Europe
* Mage 1
* P-4
* P-6
* PAP
* P80
* P120C
* P230
* Topaze
* Waxwing
* Zefiro 9
* Zefiro 23
* Zefiro 40
* India
* S7
* S9
* S12
* S139
* S200
* Iran
* Salman
* Rafe
* Israel
* LK-1
* RSA-3
* Japan
* KM-V1
* KM-V2b
* M-14
* M-24
* M-34
* M-34c
* SRB-A
* United States
* AJ-60A
* Algol
* Castor 30
* GEM
* Orbus-6
* Orbus-21
* Orion
* Space Shuttle SRB
* Star 37
* Star 48
* UA120
* SRMU
* X-248
* X-254

* * Different versions of the engine use different propellant combinations
* Engines in italics are under development

* v
* t
* e

Rocket Lab

Personnel|

* Peter Beck (founder)
* Mark Rocket (seed investor)

Products|

* Launch vehicles
* Electron
* Neutron
* Photon
* Rocket engines
* Curie
* Rutherford
* Archimedes

Facilities|

* Launch Complex 1 (NZ, Electron)
* Launch Complex 2 (US, Electron)
* Launch Complex 3 (US, Neutron)

Missions|

* Electron launches
* Venus Life Finder
* EscaPADE

* Category
* WikiCommons

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