Image credit: Convair
Image source: SDASM Archives
Flyback Booster and Orbiter
Author: G
S-72-1201-X
Image credit: McDonnell Douglas
Image source: SDASM Archives
If It’s Not Boeing, I’m Not Going
Image credit: NASA Lewis
Image source: National Archives
McDonnell Douglas Concept
NAR Space Division
I’m pretty certain these two images are by the same hand, but which one? They’re both heavily referenced and painted in what I would describe as North American Rockwell’s house style, but the palette and brushwork bring me back to a beautiful painting Don Bester did of the Saturn Shuttle. I could be wrong, but that’s the box I’m checking for now.
Image credit: North American Rockwell
Image source: Mike Acs
Mars Spacecraft
Image credit: Boeing
File source: NASA NTRS
IMIS
Image credit: Boeing
File source: NASA NTRS
From NASA-CR-67367
Image credit: General Atomics
File source: NASA NTRS
Orion Vehicles 2/2
Lunar Ferry Vehicles
Fig. 3.13 — Exploration vehicle configuration for Jupiter moon landing mission, 20-m propulsion module
Fig. 3.15 — Various payload configurations on basic 20-m propulsion module (with departure weights for given missions)
Fig. 3.16 — Earth-orbit-to-lunar-orbit ferry vehicle
Fig. 3.18 — Lunar-ferry-vehicle command module
Fig. 3.19 — Reference-design passenger module
Fig. 3.20 — Earth-orbit-to-lunar-surface ferry vehicle
Fig. 3.21 — Lunar passenger ferry
Fig. 3.22 — Lunar cargo shuttle
Fig. 3.23 — Solid-propellant-boosted earth-launched lunar logistic vehicles
Lunar Logistics Vehicles
Fig. 3.24 — S-IC boosted earth launched lunar logistics vehicle
Fig. 3.15 — Orbit launched lunar logistics vehicle
From:
Nuclear Pulse Space Vehicle Study
Vol. III — Conceptual Vehicle Designs and Operational Systems (U)
Image credit: General Atomics
File Source: Cornell
Orion Vehicles 1/2
Personnel Accommodations
Fig. 3.2 — Factors that influence the location of the shielded powered flight station
Fig. 3.4 — Powered flight station-escape vehicle for 8-man exploration missions with 10-m configurations
Fig. 3.5 — Powered flight station-escape vehicle for 20-man exploration missions with 20-m configurations
Fig 3.6 — Exploration-mission personnel accommodations for an 8-man complement
Fig 3.7 — Exploration-mission personnel accommodations for a 20-man complement
Fig 3.8 — General arrangement of payload spine and magazine payload support columns
Planetary Exploration Vehicles
Fig. 3.11 — Exploration vehicle for Mars orbital capture mission using 10-m propulsion module
Fig. 3.12 — Various payload configurations on basic 10-m propulsion module (with departure weights for 72, 850 fps Mars mission)
From:
Nuclear Pulse Space Vehicle Study
Vol. III — Conceptual Vehicle Designs and Operational Systems (U)
Image credit: General Atomics
File Source: Cornell
Space Station
Image credit: North American Rockwell
Image source: Drew Granston
