Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 02-Jul-2020

The Lockheed Aircraft Company has always had aircraft construction as its main activity, and its other activity of manufacturing engines and propulsion means is very little known.

-Lockheed had as a piston-engine subsidiary "Menasco", known as the "Menasco Manufacturing Company".

-Menasco was founded in 1926 and later became Lockheed.

C-4 Pirate
“C-4 Pirate”

-Two lines of piston engines stand out, the "Pirate" and the "Bucaneer", with the corresponding "Super Pirate" and the "Super Bucaneer".

-The top scoring engine was the "Unitwin" consisting of two coupled C6S-4 models that could be declutched. It delivered 580 hp.

Unitwin
“Unitwin”

-In the beginning, Menasco also built the Salmson radial engine under license.

-Very little known is Lockheed's pioneer jet-engine activity. Already in 1940, they began designing the L-1000 to be installed on the Canard-Lockheed L-133 fighter plane with jet propulsion.

-The project was due to N.C. Price, expert in steam turbines. In 1933 a Travel Air flew with this system.

Lockheed L-4000
“L-4000”

-The L-1000 gave 5,500 lbf of thrust. With the support received from 1943, Lockheed continues with turbojet projects, up to the L-4000, designated XJ-37-4.

-The L-1000 was officially the XJ-37-1. The XJ-35 was the L-1000 turboprop version.

-In 1945-46 Lockheed transferred the works to Menasco - its Engine Division -, but soon the project was passed to Wright, who finished the works in 1952.

LPC-156 test
“LPC-156 test”

-Another hardly known aspect is the construction of rocket engines for SRAM ballistic missiles through another Division, LPC, or Lockheed Propulsion Company.

-For example, they made the SR-13 (Solid Rocket-13) or the SR-75 on SRAM AGM-69. And many more.

-This Division was previously the "Grand Central Rocket Company", founded in 1952 and specialized in solid fuel rocket engines.

-In 1961 it became entirely Lockheed.

-The one in the previous illustration is a solid rocket in an inverted position to measure the thrust.

-It is the LPC 156 with 156 inches in diameter. It gave over 900,000 lbf of thrust.

-The best known LPC engines of the 1960’s were:

-The “Sword” giving 4,000 lbf of thrust.

-The “Viper IC” giving 5,400 lbf of thrust and the “Viper IIC” delivering 8,000 lbf of thrust.

-The “Lance II” giving 28,000 lbf.

-The Apollo engines giving 155,000 lbf.

-Various engines have been built with fuels as exotic as Polysulfide/Amonium Perchlorate.

Ionic propulsion
“Ionic propulsion”

There have been other interesting works on other propulsion systems like Ionic motors, to travel to deep space.

-Fully imaginary but original project since the nuclear reactor is 1600 meters behind the vehicle that has the ionic motors.

From Appendix 6: We received new photos of the L-1000 engine that is mentioned in the main text but could not be shown at the time.

L-1000 half-front view
Lockheed L-1000 half-rear view
"The L-1000 front and rear view"

-The L-1000 model was officially the XJ-37-1, and the L-4000 was the XJ-37-4.

Lockheed L-1000 side view
"Another view of the L-1000"

-New photograph of a Lockheed turbojet, model L-1000, which also appears in the main text.

Lockheed L-1000
“Lockheed L-1000”

-It is located at the "Planes of the Fame" Museum, in Chino, California.

-Lockheed also made rocket engines for missile propulsion, such as the solid fuel XSR13-LP-1 for the Hughes AIM-47 Falcon's air-to-air missiles.

Falcon with Lockheed engine
“Falcon with Lockheed engine”

Other Lockheed experiments were supersonic inspection and photography sounders, like the one shown below reaching a speed of 1,500 miles per hour.

Lockheed supersonic sounder
“Lockheed supersonic sounder”

-Teaming up with Northrop Grumman and Energy they have developed the CEV or “Crew Exploration Vehicle”.

CEV de Lockheed/Northrop-Grumman
“CEV Lockheed/Northrop-Grumman”

-The CEV is divided into three parts: Crew Module, Service Module and engine.

-This one has fuel tanks and two liquid rocket engines.

Engines of LOCKHEED

Model: AGM-59 , rocket engine

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: Apollo, 155,000 lbf

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: L-1000 (XJ-37) turbojet

Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 5500 Lbf
Weight:

Other details:
Model: L-4000 (XJ-37-4) turbojet

Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:

Other details:
Model: Lance II, 28000 lbf

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: Lockheed XJ-35, turboprop

Arquitecture: Turboprop
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:

Other details:
Model: LPC (from Lockheed Propulsion Div.)

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: LPC-156, rocket engine

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: SR-13 (XSR-13-LP-1)

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: SR-75

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: SRAM

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: Sword, 4000 lbf

Model: Viper IC, 5400 lbf

Model: Viper IIC, 8000 lbf

The author of this edition of Aeroengines AtoZ, through Aeroteca, collaborated on Version 2 of this video, which is presented here.

To understand the operation of the connecting rods, the 1929 Continental R 670 single-cylinder engine was chosen.

A demonstration of Version 3, improved at the author's suggestion, is also available on YouTube at a later date. This version shows bronze valve guides, improved valve spring movement, and the split crankshaft counterweights and front bearing balls also move.

The design is from Juan Soler, Sant Cugat, Barcelona

Below we show a flash of version 3

Counting also with the coloboration of JMC of Enginys Mecanics in Mataro, Barcelona