De-Orbiting/Re-Entry Phase Procedure (DG).
Hi everyone;
Since most people skip the entry phase (i cant figure why),
I did my own procedures, according with NASA's archived docs from missions,
and with space flight tech data,
These procedures are my Delta Glider Flight Standards-
Here is the Delta Glider basic procedures for
Atmosphere/Gravity De-orbiting/re-entry phase:
*Plan to Retro burn 60 degrees Longitude BEFORE the Landing site (ARP),
and add 5 degrees (tot: 65 degrees) for burn time.
Starting Altitude: 500Km/PeD = 5.300
Prograde Mode,
Retro Doors: Open,
set Auto Horizon: On / RCS Mode: LIN / AF CTRL: On,
Retro Burn (untill the descent curve reaches your Landing Site, on the MPD),
Close Retro Doors,
set LVL HORZ: Off,
Open Spoiler (keys Ctrl + B),
*Monitor the AoA (Angle of attack), ALT(altude) and SPD(speed),
Pitch: Maintain AoA +60 degrees (CRUCIAL for decreasing velocity),
References (Descent Rate);
ALT: 300Km (SPD: 6911),
ALT: 200Km (SPD: 7041),
Pitch: Maintain AoA +60 Degrees,
RCS Mode: ROT,
set MFD to HSI: ARP Rwy,
At ALT = 150Km:
Maintain pitch +60 Degrees,
At ALT = -90Km:
Lower the nose to Level with the Horizon (let it settle gently...), Pitch -3 Degrees,
At ALT = 30Km:
RCS Mode: Off,
AF CTRL: ON,
Pitch: -3 Degrees,
Let the velocity (SPD) decrease...
At ALT = 20 000m:
Level with the Horizon, Monitor the SPD,
At SPD = 500m/s: Enter Spoiler,
At SPD = 400m/s: Engines ON,
Maintain flight level (20 000m) toward ARP,
then descent/enter approach phase...
I hope this procedure will help those who like it real...
Ag1