Northrop Grumman Completes Lunar Lander Study for Golden Spike

Northrop Grumman Corporation (NYSE:NOC) has completed a feasibility study for a new commercial lunar lander for the Golden Spike Company (GSC). The study confirmed the viability of lander concepts for Golden Spike’s human lunar expedition architecture and conceived a novel new, low-mass ascent stage concept dubbed “Pumpkin.”

About Golden Spike

The Golden Spike Company (GSC) is a US-based commercial space company incorporated in 2010 with the objective of providing human expeditions to the Moon. It is named after the ceremonial final spike that joined the rails of the First Transcontinental Railroad across the United States, on May 10, 1869, and opened up the frontier to new opportunities. Golden Spike wants to sell trips to the moon to countries with less developed space capabilities but who want to take their space program to the next level.

This figure shows a preliminary sketch of the minimalist ascent pod with surface habitat concept packaged in a five-meter diameter payload fairing. The pressurized compartments and propellant tanks easily fit in the available space. Ascent thrusters are mounted on outriggers that are folded up to fit in the payload fairing and the landing gear is folded inward. Also shown are initial side and top views of the ascent pod “Pumpkin” and the surface habitat with crew members in pressure suits. (Northrop Grumman image)

Northrop Grumman’s study for Golden Spike conducted the following tasks:

Reviewed GSC’s level one requirements and synthesized a set of study ground rules and assumptions emphasizing automated operations, simplicity and low cost.

Established propulsion requirements for lunar orbit loiter, descent to the lunar surface, ascent to low lunar orbit and rendezvous with a crew vehicle for pragmatic lunar landing sites.

Developed current and stretch factors to reflect the improvement in relevant technologies since the completion of the Apollo program.

Evaluated 180 lunar lander cases for various options and sensitivities including loiter, staging, propellants, engines, surface duration, surface cargo and technology basis.

Established a pragmatic design trade space for future more detailed analysis and development.

The study determined that for GSC’s mission architecture, there are many more options for all cryogenic propellants compared with storable propellants, but that multiple storable propellant options are possible. Cryogenic propellants have higher performance, but are more difficult to contain for the GSC mission duration than storable propellants such as those used in the Apollo program.

A novel set of options using a minimalist pressurized ascent pod and descent stage with a surface habitat was also studied and shown to be viable. Layout sketches of this concept show that it can be packaged within a five-meter diameter fairing payload envelope.

Three-dimensional solid models with representative crew members established target pressurized volumes for the ascent pod and surface habitat. This unique approach has a good chance of meeting GSC’s objectives with all-storable propellants, which reduces development risks and costs.

Martin McLaughlin, Northrop Grumman’s study lead, said, “This concept has significant operability advantages for surface exploration since the surface habitat can be segmented to isolate lunar dust and provides more space for living and for selecting the most valuable lunar return samples. We affectionately call the minimalist ascent pod ‘Pumpkin’ because of its spherical shape and because it returns the crew to orbit after the surface exploration party.”

Alan Stern, president and chief executive officer, GSC, said, “Northrop Grumman has done an exemplary job and helped advance Golden Spike’s technical approach to renewed human lunar exploration. The study’s results are very exciting and will help enable a new wave of human lunar exploration that Golden Spike plans.”

Northrop Grumman and its legacy companies – Grumman Aerospace and TRW — designed and built the Apollo Lunar Module and Lunar Module Descent Engines.

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