This assembly is used for the entire journey. Applying Newton's laws to rocket motion is not only exciting, but also quite instructional. Issues to consider while constructing.
Click on image for larger view. Problems involving rocket motion illustrate how to use Newton's 2nd law when mass is not constant. Spaceplane construction is far more involved and complex than rocket design. Lets take the last stage of the rocket.
This stage has just one engine but a reduced tank-mass.
They come in a variety of sizes ranging from the the single-stage Super Arcas which stands at 7 feet to the largest, the four-stage Black Brant XII which stands 65 feet tall. A single stage rocket consists of only a single set of rocket engines and fuel containers. So this is definitly beneficial. Say they have the same structure mass, but with the two stage rocket you get to throw away a large fraction of that for the second stage. It had a proposed carbon composite structure much like the Haas 2CA. Assume that …
What if the single stage and the two stage have the same total mass. Sure, a single stage rocket could get up to space, but what about stay in space?
In June, 1944, a V2 rocket on a test flight reached beyond the karman line, the most commonly agreed upon boundary of space at 100 kms or 62 miles in altitude. Lets say for the second stage the effects of carrying an additional engine and having the reduced tank cancels out exactly. Here we will look at how high a single stage rocket will go under the influence of gravity. It fires its engine, which has an exhaust speed of v exhaust = 1.3 × 3 m/s. The part that is missing is the mass of the structure. Also say they have the same payload mass and fuel mass.
Can you show the final v is greater in the two stage? Credit: NASA The development of many NASA missions like the Compton Gamma Ray Observatory and TRACE satellite has been based on sounding rocket investigations. The V2 rocket built by Germany, were the first rockets to ever reach the edge of space. So only the first stage wouldn't be as effective. The X …
A single-stage rocket is in deep space coasting at v rocket,i = 2.4 × 10 3 m/s. The VentureStar was a single stage to orbit ship that used an Aerospike rocket engine. What is the rocket's speed v rocket,f after it has lost one-third of its inertia by exhausting burned fuel? An example stock craft which is a working single-stage-to-orbit spaceplane is the Aeris 4A.
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