OHM Space Launches Delta v150724

[OrbitHangar]

Author: crisbeta

This project recreates step by step a list of missions, with accurate insertion orbits.

Launchers used (missions/scenarios) :
- Delta IV M+(4,2) (1/6)

Before install:
- delete Config\SpaceLaunches\Delta\
- delete Config\Vessels\SpaceLaunches\Delta\
- delete Doc\SpaceLaunches\Delta\
- delete Scenarios\"Space Launches"\"By Rocket"\Delta\

Required add-ons (each mission contains in directory description required add-ons):
- Velcro Rockets v1.11 (http://www.orbithangar.com/searchid.php?ID=3388)
- Velcro EELVs v1.02 (http://www.orbithangar.com/searchid.php?ID=3462)
- MRO (http://www.orbithangar.com/searchid.php?ID=3711)

Documentation:
- Doc\SpaceLaunches\Delta\SpaceLaunchesDelta.txt

Last update:
- Launch Delta IV M+(4,2) with GPS IIF-9(1630 kg) from CCAFS SLC-37B on March 25th, 2015 18:36:00UTC. Target orbit 20,459km x 20,459km x 55deg. All scenarios to satellite separation.

Latest missions:
- Delta IV M+(4,2) with GPS IIF-9(1630 kg) from CCAFS SLC-37B on March 25th, 2015 18:36:00UTC. Target orbit 20,459km x 20,459km x 55deg.



DOWNLOAD

 

[N_Molson]

ISP 4,000 s (39,240 m/s)

Current technology ? I'm interested... :blink:

 

[crisbeta]

Pratt & Whitney J58 ([ame="http://en.wikipedia.org/wiki/J58"]Pratt & Whitney J58 - Wikipedia, the free encyclopedia[/ame])

Specific fuel consumption: 1.9 lb/(lbf-h) (wet), 0.9 lb/(lbf-h) (dry)
Maximum thrust: 34,000 pounds-force (150 kN) (wet), 25,000 pounds-force (110 kN) (dry)
Specific fuel consumption: 1.9 lb/(lbf-h) (wet), 0.9 lb/(lbf-h) (dry)

I used dry mode (110kN) 0.9lb/(lbf-h) -> 4000 s

It will be used to fly the plane to 3.3 Mach at maximum 25.9Km (SR-71 (http://en.wikipedia.org/wiki/Lockheed_SR-71_Blackbird))

 

[crisbeta]

All the comments before this post were from the old "ESA XR realistic settings" add-on which was overwritten.