Terminus of an Arc by wblack
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Description
Terminus of an Arc
An Orion’s Arm future history image.
At orbital apogee the Orion spacecraft orient prior to Mars transfer burn. They will make the crossing at 125,490 fps – a 39 day fast transfer trajectory to Mars (85,562 mph/137,700 kph).
The vehicles have shed the forward payload shroud. From this angle details of the pusher-plate, the bomb aperture (centered in the pusher-plate), and the bomb placement gun (located ahead of the pusher-plate and inside the ring of the second-stage shock absorbers) with its conical plasma shield. The first-stage shock absorbers are gas filled torridal bags – visible as black bands along the body of the pusher-plate – the two sets of shock absorbers are de-tuned in relationship to one another in order step down the powerful 150 km/sec (300,000 mph) slam of the plasma (generated by the nuclear impulse device) to something man and machine can stand.
This sequence of images depicts events in the decade before the Year Zero mark on my future history timeline – see link below.
Future History Timeline Context Link: Orion’s Arm Future History Timeline.
Related Images:
Orion Launch Vehicle Final Assembly
Right Before
Mars Settlement Project Orion Launch
Aero Braking
Syria Planum Landing
Background image courtesy NASA/JPL.
All models are my own Bryce creations, constructed in Bryce 6.3, rendered in Bryce 7 Pro.
As always thank you for your interest, thoughtful comments, and encouragement.
Comments (4)
peedy
Gorgeous image and lighting. Fantastic models. Corrie
geirla
Excellent image! Why the fast crossing for a cargo run? Wouldn't be better to use less nukes or carry more payload and make a six or nine month transit?
flavia49
outstanding
wblack
Thanks geirla, There is always a fine insight to your questions which I appreciate greatly, usually having the effect of pointing my attention to where my narrative might be lacking. The project involves construction of one hundred cargo carrying vehicles – and 10 manned transports – delivering one million tons of freight total – ten thousand tons for each launch vehicle and landing craft –to a soft touch-down on the Martian surface. Construction and launch occurs over the span of about a decade. In principal the early launches can make slower transits – with some savings on number of bombs required – so your point is spot-on – later launches, closer to the date of departure for the manned transports, make the faster transits.