Transorbital Technology - Mission

Professional Narrative
Shuttle Optimization
Asonic O2H2 transients
Asonic CH4 transients
Pogo transients
Asonic aerobody
Trisonic aerobody
Grand Forks 1988
Adaptive Spaceplane

Charl E Janeke - Asonic H2/C4H8 Corollary

													77%	23%
cj: 970825;8/98													6O2	C4H8=	4CO2	4H2O
													192	56	sum=	248

Time	Time	mass	H2+O2	%H2	H2/thst	HC+O2	A/fac	%	HC/thst	Tot/thst	Acc	Vel	%	H.dist	fact	Hight
(sec)	(min)	(lb)	0.6	thst	360	0.4	3.3	O2	225	H2+HC	xg	ft/sec	mass	*1000	0.87	*10ft
			60			228	0.96		250
			lb/sec			lb/sec
0	0	100000	60000	100	21600	40000	3.30	33	169290	190890	1.9	0	100	0	1	0
1	0	99712	59940	100	21600	39772	3.15	37	161395	182995	1.8	61	100	0.0	0.87	3
2	0	99424	59880	100	21600	39544	3.01	42	154163	175763	1.8	121	99	0.1	0.76	11
3	0	99136	59820	100	21600	39316	2.88	45	147525	169125	1.7	177	99	0.2	0.66	27
4	0	98848	59760	100	21600	39088	2.76	49	141421	163021	1.6	232	99	0.4	0.57	52
5	0	98560	59700	100	21600	38860	2.65	52	135800	157400	1.6	286	99	0.6	0.50	84
6	0	98272	59640	100	21600	38632	2.55	55	130614	152214	1.5	337	98	0.9	0.43	123
7	0	97984	59580	100	21600	38404	2.45	58	125821	147421	1.5	387	98	1.2	0.38	168
8	0	97696	59520	100	21600	38176	2.37	60	121386	142986	1.5	435	98	1.5	0.33	217
9	0	97408	59460	100	21600	37948	2.29	62	117275	138875	1.4	482	97	1.9	0.29	270
10	0	97120	59400	100	21600	37720	2.21	65	113460	135060	1.4	528	97	2.2	0.25	326
20	0	94240	58800	100	21600	35440	2.14	67	109914	131514	1.4	976	94	9.0	0.22	520
30	1	91360	58200	100	21600	33160	2.08	69	106614	128214	1.4	1425	91	20	0.19	902
40	1	88780	57900	50	10800	30880	2.02	70	103540	114340	1.3	1877	89	33	0.16	1445
50	1	86200	57600	50	10800	28600	1.96	72	100672	111472	1.3	2292	86	52	0.14	2186
60	1	83620	57300	50	10800	26320	1.91	73	97993	108793	1.3	2708	84	75	0.12	3120
70	1	81040	57000	50	10800	24040	1.86	75	95489	106289	1.3	3127	81	103	0.11	4234
80	1	78460	56700	50	10800	21760	1.82	76	93145	103945	1.3	3550	78	137	0.09	5514
90	2	75880	56400	50	10800	19480	1.77	77	90949	101749	1.3	3976	76	175	0.08	6939
100	2	73300	56100	50	10800	17200	1.73	79	88890	99690	1.4	4408	73	219	0.07	8493
125	2	66850	55350	50	10800	11500	1.70	80	86956	97756	1.5	5503	67	368	0.06	10763
150	3	60400	54600	50	10800	5800	1.66	81	85140	95940	1.6	6680	60	575	0.05	13852
175	3	53950	53850	50	10800	100	1.63	82	83432	94232	1.7	7959	54	861	0.05	17875
200	3	52350	52350	100	21600	0	0.00		0	21600	0.4	9365	52	266	0.04	18955
230	4	50550	50550	100	21600	0	0.00		0	21600	0.4	9763	51	364	0.04	20242
260	4	48750	48750	100	21600	0	0.00		0	21600	0.4	10176	49	482	0.03	21725
290	5	46950	46950	100	21600	0	0.00		0	21600	0.5	10604	47	623	0.03	23392
320	5	45150	45150	100	21600	0	0.00		0	21600	0.5	11049	45	789	0.02	25228
350	6	43350	43350	100	21600	0	0.00		0	21600	0.5	11511	43	983	0.02	27219
380	6	41550	41550	100	21600	0	0.00		0	21600	0.5	11992	42	1209	0.02	29349
416	7	39390	39390	100	21600	0	0.00		0	21600	0.5	12595	39	1528	0.02	31691
452	8	37230	37230	100	21600	0	0.00		0	21600	0.6	13230	37	1908	0.01	34236
488	8	35070	35070	100	21600	0	0.00		0	21600	0.6	13903	35	2361	0.01	36977
524	9	32910	32910	100	21600	0	0.00		0	21600	0.7	14617	33	2901	0.01	39906
560	9	30750	30750	100	21600	0	0.00		0	21600	0.7	15378	31	3547	0.01	43021
596	10	28698	28698	95	20520	0	0.00		0	20520	0.7	16192	29	4089	0.01	46146
632	11	26754	26754	90	19440	0	0.00		0	19440	0.7	17021	27	4673	0.01	49252
668	11	24918	24918	85	18360	0	0.00		0	18360	0.7	17863	25	5293	0.01	52314
704	12	23190	23190	80	17280	0	0.00		0	17280	0.7	18717	23	5946	0.01	55306
740	12	21570	21570	75	16200	0	0.00		0	16200	0.8	19581	22	6621	0.00	58204
776	13	20058	20058	70	15120	0	0.00		0	15120	0.8	20452	20	7308	0.00	60988
812	14	18654	18654	65	14040	0	0.00		0	14040	0.8	21325	19	7990	0.00	63635
848	14	17358	17358	60	12960	0	0.00		0	12960	0.7	22198	17	8644	0.00	66127
884	15	16170	16170	55	11880	0	0.00		0	11880	0.7	23063	16	9244	0.00	68445
920	15	15090	15090	50	10800	0	0.00		0	10800	0.7	23915	15	9753	0.00	70573
950	16	14280	14280	45	9720	0	0.00		0	9720	0.7	24606	14	9890	0.00	72451
														alt.	miles	126