Skip to content

Station E05

  • artist
  • gallery
  • collection
  • featured
  • index

0025-bx092-fd004_006

source

Mars Capture Mission in 1982. Orbit crew inspects the nuclear twin engine NERVA II system of the Earth Departure Module. Each engine delivers 250, 000 lbs. of thrust.

Image credit: Krafft Ehricke Papers
Image source: NASM

Share this:

  • Click to share on X (Opens in new window) X
  • Click to share on Tumblr (Opens in new window) Tumblr
  • Click to share on Pinterest (Opens in new window) Pinterest
  • Click to share on Pocket (Opens in new window) Pocket
  • Click to email a link to a friend (Opens in new window) Email
Like Loading...
Unknown's avatarAuthor GPosted on March 28, 2022March 26, 2025Categories Krafft Arnold Ehricke PapersTags Earth Departure Module, EDM, EMPIRE - General Dynamics, Future Nuclear Rockets, General Dynamics, General Dynamics EMPIRE, Heliocentric Interorbital Space Vehicle, HISV, Interorbital Space Vehicle, ISV, Krafft Arnold Ehricke Papers, Krafft Arnold Ehricke Papers, Krafft Ehricke, Mars Capture Mission, NASM, National Air and Space Museum, National Air and Space Museum Archives, NERVA, NERVA II, NTR, nuclear rocket, Nuclear Thermal Rocket, Solar Transport

Leave a comment Cancel reply

Post navigation

Previous Previous post: Vehicle Requirements
Next Next post: Solar Transportation
  • artist
  • gallery
  • collection
  • featured
  • index
Station E05 Website Built with WordPress.com.
 

Loading Comments...
 

    %d