Big dumb booster


Big Dumb Booster is a general class of launch vehicle based on the premise that it is cheaper to operate large rockets of simple design than it is to operate smaller, more complex ones regardless of the lower payload efficiency. As referred to by the Office of Technology Assessment:
Even though the large minimum-cost design booster is less efficient for all around operation, its total cost of operation is cheaper because it is easier to build, operate and maintain, with the benefit of high reliability because of reduced parts counts.

History

Concept work was led by proponents at Aerospace Corporation, TRW, and Aerojet General, beginning in the late 1950s. The typical approach included maraging steel for structure, pressure-fed engines using / UDMH, later LOX /RP-1, with pintle injectors scaled up from TRW's Lunar Module Descent Engine.
The Sea Dragon was an extremely large BDB/MCD 2-stage launch vehicle defined by Robert Truax and others at Aerojet. Space Technology Laboratories, Inc. contributed to the design effort. It was to be able to carry a payload of over 500 metric tons into low Earth orbit.
TRW developed and fired several engines, including their TR-106, a robust, low-cost engine of 2890 kN thrust to demonstrate the engine technology readiness. TRW also defined a low-cost shuttle-surrogate booster to launch 29 metric tons into a 28-degree orbit at a cost of about $59 million.
Beal Aerospace furthered the quintessential BDB/MCD with their BA-1 and BA-2 launch vehicles.

Minimum cost design

The MCD methodology was developed by Arthur Schnitt. It is a process of making trade analyses to understand the cost versus mass implications. It is not a specific design choice like pressure-fed engines or single engine per stage. The process shows how to reduce costs by allowing mass to increase where there is a favorable impact on life-cycle cost. Some of the early design concepts were referred to as big dumb boosters, not necessarily in a favorable manner.