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- The Rocket category groups pages related to rocket systems design, flight environment and parameters, design and modelling. ...7 members (0 subcategories, 0 files) - 00:58, 29 December 2012
...a, mass ratio or Isp and Delta V, and computes the dry and wet mass of the rocket. Each subsystem's mass is evaluated and the formulas are simple enough to b The rocket is modelled as depicted below: ...(21 KB) - 01:42, 12 December 2012- Graph of the rocket trajectory for first moments after release, assuming ignition at the time o ...03:10, 27 November 2012
- Rocket model illustration for the computed rocket model: [[File:Rocket_mass.c]] ...00:26, 11 December 2012
- Schematic rocket trajectory to explain initial and final direction vectors and atmosphere cr ...21:28, 25 January 2010
- =Rocket aerodynamics= ...tage air-to-orbit configuration, when aerodynamic effects are ignored. The rocket engine has to be larger to compensate the gravity. ...5 KB (815 words) - 00:16, 12 March 2013
BOOK: HOW to DESIGN, BUILD and TEST SMALL LIQUID-FUEL ROCKET ENGINES Backup archive from http://www.risacher.org/rocket/ ...(278 KB) - 04:09, 29 December 2010- ...lar systems of existing rocket engines can be found in the [[RocketEngines|rocket engines]] page. =First mass approximation for our rocket= ...29 KB (4,729 words) - 01:08, 29 December 2012
- =Rocket Fuel tanks= ...nd one for the oxidizer, but it has not always been the case. The Redstone rocket for example used a single tank with an internal separation, as we can see b ...8 KB (1,251 words) - 01:13, 29 December 2012
- tank model for rocket mass version >= 3 ...01:37, 9 November 2012
- tank model for rocket mass versions 1 and 2 ...01:36, 9 November 2012
- (13 KB) - 02:01, 24 November 2012
Page text matches
- Rocket model illustration for the computed rocket model: [[File:Rocket_mass.c]] ...00:26, 11 December 2012
- The Rocket category groups pages related to rocket systems design, flight environment and parameters, design and modelling. ...7 members (0 subcategories, 0 files) - 00:58, 29 December 2012
- tank model for rocket mass version >= 3 ...01:37, 9 November 2012
- tank model for rocket mass versions 1 and 2 ...01:36, 9 November 2012
- Schematic rocket trajectory to explain initial and final direction vectors and atmosphere cr ...21:28, 25 January 2010
- (Single-Spent-to-orbit), like a rocket, and thus using the £1,000 for the full rocket or a Helium balloon. Everything that is recovered and reusable doesn't ...1 KB (194 words) - 00:06, 20 November 2010
- BOOK: HOW to DESIGN, BUILD and TEST SMALL LIQUID-FUEL ROCKET ENGINES Backup archive from http://www.risacher.org/rocket/ ...(278 KB) - 04:09, 29 December 2010
- Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio. ...20:08, 11 December 2012
- Graph representing rocket dry and wet mass as function of the payload mass (or any other fixed mass s ...20:02, 11 December 2012
- Graph representing rocket dry and wet mass as function of the mass ratio (fixed by Isp and Delta V). ...20:09, 11 December 2012
- Graph representing rocket dry and wet mass as function of the payload mass (or any other fixed mass s ...19:57, 11 December 2012
- Graph representing rocket dry and wet mass as function of the vehicle (overall) initial thrust-to-wei ...20:06, 11 December 2012
- Graph representing rocket dry and wet mass as function of the Delta V. Done with version 3 of [[File: ...20:53, 11 December 2012
- Wings will have to sustain the mass of the rocket at accelerations from -2g to +4g. They will have to support heavy curving, ===Rocket body=== ...5 KB (843 words) - 11:52, 23 October 2010
- Graph of the rocket trajectory for first moments after release, assuming ignition at the time o ...03:10, 27 November 2012
- ...a, mass ratio or Isp and Delta V, and computes the dry and wet mass of the rocket. Each subsystem's mass is evaluated and the formulas are simple enough to b The rocket is modelled as depicted below: ...(21 KB) - 01:42, 12 December 2012
- ** RocketEngines|Rocket engine ...271 bytes (25 words) - 02:01, 13 December 2012
- ...lift-off operation. An additional disposable tank could be mounted on the rocket or on the aircraft, jettisoned after this burn. The engine may allow thrott * push-on boosters, either with propellers or miniature solid rocket engines, that would stay on the ground when the plane lifts-off. ...6 KB (982 words) - 19:23, 5 November 2012
- ...lable documentation on the numerous subjects linked the project, including rocket science, turbofans, aerodynamics, amateur rocketry and SSTO. ...m/ Opennautics] (European project) develops a hybrid engine for an amateur rocket, all open source. ...6 KB (923 words) - 14:04, 31 December 2013
- Graph representing rocket dry and wet mass as function of the Isp. This is clearly exponential on the ...20:59, 11 December 2012
