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S-550

S-550 is a science topic covered in the lgStudy science library. This page brings together a partial reference excerpt, illustrations, worked examples, real-world applications and a short study plan, so you can understand S-550 rather than just read about it. In short: The S-550 was a proposed crewed space capsule, designed in 2005–06 at Venturer Aerospace, in response to the NASA Commercial Orbital Transportation Services (COTS) program to provide commercial resupply and logistics support for the International Space Station after the retirement of the Space Shuttle. It was an outgrowth of earlier Venturer Aerospace crewed capsule research and development projects.

S-550 — main illustration
S-550 — illustration

Key takeaways

  • S-550 belongs to science; place it in that map before memorising details.
  • Learn the definition first, then one example that makes the definition concrete.
  • Connect S-550 to a quantity you can measure, compute or draw — that is where exam questions come from.
  • Reproduce the core statement of S-550 from memory before moving on to harder problems.

Reference excerpt

The S-550 was a proposed crewed space capsule, designed in 2005–06 at Venturer Aerospace, in response to the NASA Commercial Orbital Transportation Services (COTS) program to provide commercial resupply and logistics support for the International Space Station after the retirement of the Space Shuttle. It was an outgrowth of earlier Venturer Aerospace crewed capsule research and development projects. NASA did not select the design for further funded development, and the company has not to date proceeded to develop the vehicle with private funding. Venturer Aerospace did not participate in the second COTS program round in 2007.

Description

The S-550 capsule was intended to carry up to six people (normally 2 or 3) and significant internal and external cargo on resupply missions to the International Space Station (ISS). Unlike the other COTS competitors, the S-550 capsule was explicitly a human-operated vehicle - while it had automated flight functions, it was intended to be flown with crews for any space station mission, with the crew in control for all rendezvous and dockings with ISS.

Design The overall vehicle was design was for a 3.0 m (10 ft)-diameter ballistic capsule, weighing 7,500 kilograms (16,500 lb) including payloads. The capsule was projected to weigh 3,059 kg (6,744 lb) "wet" (with 2 crew and consumables, but not cargo), the service module 1,755 kg (3,869 lb) "wet" including rocket propellants, and 2,300 kg (5,100 lb) of internal cargo or passengers within the capsule. Additional mass in external unpressurized cargo could be obtained with increased launch vehicle capacity beyond 7,500 kg or by trading off internal cargo for external cargo.

Capsule shape The S-550 capsule is a sphere-cone type lifting ballistic space capsule, similar to the shape of the film capsule reentry modules in the Corona spy satellite, but much larger. The general shape was also used by COTS competitor T/Space's CXV capsule. The capsule design shape had a spherical nose section diameter of 0.8 of the base diameter and 10 degree conical half-angle (see Atmospheric reentry).

Capsule layout The capsule consisted of two structures - an outer aeroshell, which supported the ablative heatshield (thermal protection system), and an inner pressurized cylinder containing the crew, systems, and cargo space. Most of the spacecraft systems were at the front of the cylinder, up against the front bulkhead. The crew were seated in one row near the rear bulkhead and access hatch, with 2 "crew" seats on the sides with flight controls on the rear bulkhead and one passenger in the middle. Cargo was carried in the middle of the capsule, at the capsule's center of gravity, to simplify loading effects on reentry angles and lift.

Descent and landing The S-550 capsule was intended to descend under a parachute system and touch down on land, using an inert aluminum foam crush structure in the nose of the capsule to attenuate the roughly 7 meter per second touchdown velocity. The landing did not require any active controls or systems to operate safely. Emergency landings in the water were handled by capsule flotation systems.

Service module The service module was intended to provide rocket thrusters to control spacecraft attitude and provide orbital maneuvering capability to rendezvous with the International Space Station and then reenter the Earth's atmosphere. It included some structure, propellant tanks, and rocket motor systems.

References

Worked examples

Example 1 — a first encounter with S-550

Start with the simplest possible case. Write down what S-550 claims or describes in one sentence, then invent the smallest concrete situation in which that sentence is true. In science, the smallest case is usually a single object, a single equation or a single measurement. Check that every symbol or term in your sentence has a meaning in that case.

Example 2 — changing one variable

Take the situation from Example 1 and change exactly one quantity: double it, halve it, or set it to zero. Predict what should happen to S-550 before you calculate. Comparing your prediction with the result is the fastest way to find out whether you understand the idea or only the words.

Example 3 — an exam-style question

Typical questions about S-550 ask you to (a) state it precisely, (b) apply it to given data, and (c) explain a limitation. Practise writing all three answers in under five minutes; the third part is what separates a full-mark answer from an average one.

Applications of S-550

In research
S-550 appears in science research whenever the underlying quantities have to be modelled precisely. Papers usually cite it as a starting assumption and then explore where it breaks down.
In technology and industry
Engineering practice reuses S-550 in design rules, simulations and safety margins. Knowing the idea lets you read a specification sheet and understand why the numbers look the way they do.
In the classroom
S-550 is common in secondary-school and first-year university syllabi. It links to neighbouring topics Crewed spacecraft, Proposed spacecraft, so understanding it makes those chapters shorter.
In everyday life
Look for S-550 outside the textbook — in sport, cooking, traffic, electronics or the sky above you. An example you found yourself is remembered far longer than one you were given.
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How to study S-550 in 20 minutes

  1. Read the reference excerpt below once, without taking notes.
  2. Close the page and write down what S-550 means in your own words.
  3. Compare your version with the excerpt and mark what you missed.
  4. Work through the three examples above with pen and paper.
  5. Explain S-550 out loud to somebody else — or to Teacher Smith in the lgStudy chat.

Frequently asked questions

What is S-550 in simple terms?

The S-550 was a proposed crewed space capsule, designed in 2005–06 at Venturer Aerospace, in response to the NASA Commercial Orbital Transportation Services (COTS) program to provide commercial resupply and logistics support for the International Space Station after the retirement of the Space Shut…

Why does S-550 matter?

Because it connects several science ideas at once: it gives you a definition you can apply, a quantity you can calculate, and a way to check whether a result is plausible.

How should I study S-550?

Read the excerpt, restate it from memory, then work through the examples and applications listed on this page. The five-step study plan above takes about twenty minutes.

What does this page cover?

It gives you a compact reference excerpt plus original lgStudy explanations, examples, applications and study material on S-550.

Tags

  • Crewed spacecraft
  • Proposed spacecraft

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