For example, an observer will see a ball fall the same way in a rocket ( left ) as it does on Earth ( right ), provided that the acceleration of the rocket provides the same relative force.

For the five 6. 4 meganewton sea-level thrust F-1 rocket engines of the Saturn V, burning together, the reaction generated roughly 1. 62 × 10 < sup > 11 </ sup > watts ( J / s ) ( 162 gigawatt ) or 217 million horsepower.

For example: bunny hopping or strafe jumping can be used to move faster than normal, while rocket jumping enables the player to reach otherwise-inaccessible areas at the cost of some self-damage.

For example, from the equation, with an of 0. 7, a rocket flying at Mach 0. 85 ( which most aircraft cruise at ) with an exhaust velocity of Mach 10, would have a predicted overall energy efficiency of 5. 9 %, whereas a conventional, modern, air-breathing jet engine achieves closer to 35 % efficiency.

For pure rocket approaches Tsiolkovsky's rocket equation shows that dead weight will prevent reaching orbit unless the ratio of propellant to structural mass ( called mass ratio ) is very high — between about 10 and 25 ( i. e. 24 parts propellant weight to 1 part structural weight ; depending on propellant choice ).

For example, a pulley made of unobtainium might be massless and frictionless ; however, if used in a nuclear rocket, unobtainium would be light, strong at high temperatures, and resistant to radiation damage.

For example, the Titan IIIC solid boosters injected nitrogen tetroxide for LITV ; the tanks can be seen on the sides of the rocket between the main center stage and the boosters.

For vertical launch of a rocket the initial thrust must be more than the weight.

For example, the experimental rocket plane SpaceShipOne was designed without any use of wind tunnels.

For a chemical rocket the propellant mass therefore would include both fuel and oxidizer ; for air-breathing engines only the mass of the fuel is counted, not the mass of air passing through the engine.

For example, an unhandled arithmetic overflow in the engine steering software was the primary cause of the crash of the maiden flight of the Ariane 5 rocket.

For the first attempt, in a 2003 pilot episode, the crew replicated the scene and the thrust of the JATO with some commercially-available amateur rocket motors.

For example, a mixture of lithium, hydrogen, and fluorine produced a specific impulse of 546 seconds ; the highest ever of any chemical rocket motor.

For Daedalus, this process was run within a large electromagnet which formed the rocket engine.

For the Apollo lunar missions, the restartable J-2 engine in the third ( S-IVB ) stage of the Saturn V rocket performed TLI.

For sustained operation, rocket propulsion can be used, which by its nature adds gas at high pressure to the cavitation bubble.

For more than half a century, the facility and its personnel, teamed together with government and industrial partners, have provided the United States with rocket propulsion that fits the needs of the nation and anticipates the future of propulsion technology.

For the same reasons a new type of Walter rocket was envisioned, a modification of the engine in the Me 163 that would burn coal-gas ( benzine ) instead of the hydrogen peroxide used in other Walter designs ( although a small amount of peroxide was used to drive the fuel pumps ).

For example: the 15 % efficiency advantage of Soviet rocket engines which used exhaust gases to power the fuel pumps, or of the Squall supersonic cavitation torpedo.

: For the launch vehicle of the same name see Soyuz ( rocket family )

For example, the Proton M uses a set of four intermediate orbits, requiring five rocket firings, to place a satellite into GEO from the high-inclination site of Baikonur Cosmodrome, in Kazakhstan.

For each class of application ( e. g., audio, video ), RTP defines a profile and one or more associated payload formats.

For example NASA's space shuttle fires its engines for around 8. 5 minutes, consuming 1, 000 tonnes of solid propellant ( containing 16 % aluminium ) and an additional 2, 000, 000 litres of liquid propellant ( 106, 261 kg of liquid hydrogen fuel ) to lift the 100, 000 kg vehicle ( including the 25, 000 kg payload ) to an altitude of 111 km and an orbital velocity of 30, 000 km / h.

For rocket-powered SSTO, the main challenge is achieving a high enough mass-ratio to carry sufficient propellant to achieve orbit, plus a meaningful payload weight.

For air-breathing SSTO, the main challenge is system complexity and associated research and development costs, material science, and construction techniques necessary for surviving sustained high-speed flight within the atmosphere, and achieving a high enough mass-ratio to carry sufficient propellant to achieve orbit, plus a meaningful payload weight.

For example, in Ethernet the maximum frame size 1526 bytes ( maximum 1500 byte payload + 8 byte preamble + 14 byte header + 4 Byte trailer ).

For instance, if limited onboard power fed to its engine was the dominant limitation on how much payload a hypothetical spacecraft could shuttle ( such as if intrinsic propellant economic cost was minor from usage of extraterrestrial soil or ice ), ideal exhaust velocity would rather be around 62. 75 % of total mission delta v if operating at constant specific impulse, except greater optimization could come from varying exhaust velocity during the mission profile ( as possible with some thruster types, including mass drivers and variable specific impulse magnetoplasma rockets ).

For STS-1, the frame is transmitted as three octets of overhead, followed by 87 octets of payload.

For STS-1, the payload is referred to as the synchronous payload envelope ( SPE ), which in turn has 18 stuffing bytes, leading to the STS-1 payload capacity of 756 bytes.

For example, a bit-wise example of a IEEE floating-point standard single precision ( 32-bit ) NaN would be: < span style =" white-space: nowrap ;"> s111 1111 1axx xxxx xxxx xxxx xxxx xxxx </ span > where s is the sign ( most often ignored in applications ), a determines the type of NaN, and x is an extra payload ( most often ignored in applications ).

For example, a payload might covertly steal user passwords, credit card information, computing resources, or conduct other unauthorized activities.

For proper functioning of these experiments, the payload requires an ORU ( Orbital Replacement Unit ) which consists of the EPS ( Electrical Power System ), CT ( Communications & Tracking ) and the TCS ( Thermal Control System ).

For this reason the useful load fraction calculates a similar number, but based on the combined weight of the payload and fuel together.

For spacecraft the payload fraction is often less than 1 %, while the useful load fraction is perhaps 90 %.

For the first payload, any information that the virus has overwritten with zeros is lost.

For the special episode, a cardboard Spitfire called " Jet 1000 " was used, which had its categories listed on a series of bombs coming out from it on pieces of string ( referred to by Bob as its " payload "), while the others were written on the wings.

For STS-39, only the payload in the Multi-Purpose Experiment Canister ( MPEC ) was listed as classified.

For STS-95, a single-module Spacehab flew in the forward portion of Discovery's payload bay with the crew gaining access to the module through the airlock tunnel system.

For example, writing a fixed-size header and its associated payload data that are placed non-sequentially in memory can be done by a single vectored I / O operation without first concatenating the header and the payload to another buffer

For the first time, the IAEA report outlines, in depth, the country ’ s detonator development, the multiple-point initiation of high explosives, and experiments involving nuclear payload integration into a missile delivery vehicle.

For sub-orbital missions the payload can be either a recoverable vehicle of up to 720 kg or research equipment placed in a descent vehicle of up to 400 kg.

For technical reasons, the payload was launched upside down.