Image credit: Lockheed
File source: NASA NTRS
19730024037
Tag: Lockheed
Baseline Vehicle System (LS 200-5)
Image credit: Lockheed
File source: NASA NTRS
LS 400-7
Image credit: Lockheed
File source: NASA NTRS
LS 200-8
Image credit: Lockheed
File source: NASA NTRS
LS 400-6
Image credit: Lockheed
File source: NASA NTRS
LS 400-6 2-Stage
Image credit: Lockheed
File source: NASA NTRS
LS 200-8
Image credit: Lockheed
File source: NASA NTRS
Manned Orbiting Laboratory
Planetary Illustrations (artists’ concepts)
Image credit: Krafft Ehricke Papers / Lockheed
Image source: NASM
LMSC Photo
Image credit: Lockheed
Image source: Mike Acs
Chandra X-ray Observatory
Image credit: NASA/SAO
Image source: Chandra X-Ray Observatory
Configuration Development Study
Baseline Vehicle Sizing
B-52 Clearances and Constraints
B-52 Clearances and Constraints
B-52 Constraints Physical Space Available
X-24C/B-52 Interface
Ablator Surface Area – Mach 6/1033K
Image credit: Lockheed Martin
File source: NASA NTRS
