RetroSearch Browse

Home - News ( United States | United Kingdom | Italy | Germany ) - Football scores

Showing content from http://www.astronautix.com/c/../s/../s/star37xfp.html below:

Star 37XFP

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Star 37XFP Part of Star 37 Thiokol solid rocket engine. In Production. Orbit insertion motor qualified for Global Positioning Satellite. Used as a replacement for the discontinued STAR 37F. Propellant: 884 kg of AP/HTPB/Al in 6Al-4V titanium case. AKA: 66-KS-8,550;TE-M-714-16/17. Status: In Production. Number: 16 . Thrust: 31.50 kN (7,081 lbf). Gross mass: 955 kg (2,105 lb). Unfuelled mass: 71 kg (156 lb). Specific impulse: 290 s. Burn time: 66 s. Height: 1.52 m (4.97 ft). Diameter: 0.93 m (3.06 ft). Orbit insertion motor configuration was qualified for Rockwell International's Global Positioning Satellite, and the TE-M-714-17 configuration was qualified as the apogee motor for the RCA SATCOM Ku band satellite. This motor can be used as a replacement for the discontinued STAR 37F motor. Propellant: 884 kg of AP/HTPB/Al in 6Al-4V titanium case. Casing: semi-submerged, contour nozzle has a carbon/carbon throat insert, and the aft end igniter is. remotely initiated. Total impulse 258,660 kgf-s. Propellant mass fraction 0.925. Propellant Formulation: HTPB. Country: USA. Propellants: Solid. Stages: Star 37XFP. Agency: Thiokol. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

RetroSearch is an open source project built by @garambo | Open a GitHub Issue

Search and Browse the WWW like it's 1997 | Search results from DuckDuckGo

HTML: 3.2 | Encoding: UTF-8 | Version: 0.7.4